Optimal trajectories and normal load analysis of hypersonic glide vehicles via convex optimization
Hypersonic trajectory optimization has been intensively investigated through different approaches; however, the normal-load-optimal entry problems were barely studied and reported in the literature. Finding the optimal trajectories with maximum or minimum peak normal load is essential to evaluate th...
Uložené v:
| Vydané v: | Aerospace science and technology Ročník 87; s. 357 - 368 |
|---|---|
| Hlavný autor: | |
| Médium: | Journal Article |
| Jazyk: | English |
| Vydavateľské údaje: |
Elsevier Masson SAS
01.04.2019
|
| Predmet: | |
| ISSN: | 1270-9638, 1626-3219 |
| On-line prístup: | Získať plný text |
| Tagy: |
Pridať tag
Žiadne tagy, Buďte prvý, kto otaguje tento záznam!
|
| Abstract | Hypersonic trajectory optimization has been intensively investigated through different approaches; however, the normal-load-optimal entry problems were barely studied and reported in the literature. Finding the optimal trajectories with maximum or minimum peak normal load is essential to evaluate the maneuverability and structural strength of the vehicle. In this paper, both the maximum and minimum peak-normal-load entry trajectories are explored using convex optimization. Based on the previous work, the maximum-peak-normal-load entry problem is firstly addressed by a Big-M method and a line-search approach. Through successive relaxations, the nonconvex discrete-event optimal control problem associated with maximum-peak-normal-load entry is transformed into a sequence of mixed-integer convex optimization problems. Then, a line-search technique is introduced to improve the convergence of the proposed method. Additionally, a sequential convex programming method is designed to solve the minimum-peak-normal-load entry problem to comprehensively analyze the normal load during the entry flight. There are efficient solvers that can solve each relaxed convex subproblem with a global optimum if the feasible set of the subproblem is nonempty. The convergence and accuracy of the proposed methodologies are demonstrated by numerical simulations, and the feasibility of the converged solutions is discussed based on an entry-corridor approach. |
|---|---|
| AbstractList | Hypersonic trajectory optimization has been intensively investigated through different approaches; however, the normal-load-optimal entry problems were barely studied and reported in the literature. Finding the optimal trajectories with maximum or minimum peak normal load is essential to evaluate the maneuverability and structural strength of the vehicle. In this paper, both the maximum and minimum peak-normal-load entry trajectories are explored using convex optimization. Based on the previous work, the maximum-peak-normal-load entry problem is firstly addressed by a Big-M method and a line-search approach. Through successive relaxations, the nonconvex discrete-event optimal control problem associated with maximum-peak-normal-load entry is transformed into a sequence of mixed-integer convex optimization problems. Then, a line-search technique is introduced to improve the convergence of the proposed method. Additionally, a sequential convex programming method is designed to solve the minimum-peak-normal-load entry problem to comprehensively analyze the normal load during the entry flight. There are efficient solvers that can solve each relaxed convex subproblem with a global optimum if the feasible set of the subproblem is nonempty. The convergence and accuracy of the proposed methodologies are demonstrated by numerical simulations, and the feasibility of the converged solutions is discussed based on an entry-corridor approach. |
| Author | Wang, Zhenbo |
| Author_xml | – sequence: 1 givenname: Zhenbo orcidid: 0000-0002-8979-9765 surname: Wang fullname: Wang, Zhenbo email: zwang124@utk.edu organization: Mechanical, Aerospace and Biomedical Engineering Department, The University of Tennessee, Knoxville, TN 37996, USA |
| BookMark | eNp9kMlOwzAQQC1UJNrCB3DzDyR4ySpOqGKTKvUCZ2tiT6ijEFd2FFG-Hody4tDTLJo3mnkrshjcgITccpZyxou7LoUwpoLxOmUyZUxckCUvRJFIwetFzEXJkrqQ1RVZhdCxOFFnYkma3WG0n9DT0UOHenTeYqAwGDo4P_d7BybW0B-DDdS1dH88oA9usJp-9NYgnXBvdR-pyQLVbpjwi7p5q_2G0brhmly20Ae8-Ytr8v70-LZ5Sba759fNwzbRoi7HpM7BCIEVz-JlkDe1kVVbYd5IUTY55thoyBg0LXLT5AZaEBUWDExRSAZFJteEn_Zq70Lw2KqDj6_5o-JMzZJUp6IkNUtSTKqoIDLlP0bb8ffq6MP2Z8n7E4nxpcmiV0FbHDQa66NHZZw9Q_8ARICHCg |
| CitedBy_id | crossref_primary_10_1155_2021_8827377 crossref_primary_10_1109_TAES_2020_3015321 crossref_primary_10_1016_j_ast_2021_107132 crossref_primary_10_1016_j_arcontrol_2021_04_013 crossref_primary_10_1108_AEAT_11_2019_0221 crossref_primary_10_1016_j_ast_2022_107733 crossref_primary_10_1177_09544100221127058 crossref_primary_10_1016_j_paerosci_2021_100696 crossref_primary_10_1016_j_jer_2024_07_014 crossref_primary_10_1016_j_ast_2024_109636 crossref_primary_10_1155_2021_2526916 crossref_primary_10_1002_oca_2839 crossref_primary_10_1016_j_asr_2025_05_051 crossref_primary_10_1016_j_ast_2025_110542 crossref_primary_10_1109_ACCESS_2020_2997235 crossref_primary_10_1016_j_ast_2024_109346 crossref_primary_10_1016_j_ast_2019_105427 crossref_primary_10_1016_j_ast_2024_109349 crossref_primary_10_1016_j_ast_2024_109464 crossref_primary_10_1016_j_ast_2022_107842 crossref_primary_10_1016_j_ast_2020_105756 crossref_primary_10_1016_j_ast_2020_106448 crossref_primary_10_3390_math12091306 crossref_primary_10_2514_1_G006237 crossref_primary_10_1016_j_ast_2019_105433 crossref_primary_10_1016_j_ast_2021_107234 crossref_primary_10_3390_aerospace11090785 crossref_primary_10_1109_TIE_2024_3398674 crossref_primary_10_1016_j_ast_2022_108006 crossref_primary_10_1155_2021_3676810 crossref_primary_10_1016_j_ast_2021_106946 crossref_primary_10_1016_j_ast_2020_105841 crossref_primary_10_3390_aerospace9030149 crossref_primary_10_1016_j_cja_2025_103656 crossref_primary_10_1109_TAES_2020_3037417 crossref_primary_10_1016_j_ast_2020_105682 crossref_primary_10_1016_j_ast_2020_106374 crossref_primary_10_1016_j_cja_2021_06_020 crossref_primary_10_1155_2019_2065730 crossref_primary_10_3390_aerospace9040188 crossref_primary_10_1016_j_ast_2021_107283 crossref_primary_10_1049_rsn2_12400 crossref_primary_10_1016_j_ast_2021_107166 crossref_primary_10_1109_ACCESS_2021_3137641 crossref_primary_10_3390_drones8120709 crossref_primary_10_3390_math11020288 crossref_primary_10_2514_1_G004874 crossref_primary_10_1016_j_ast_2024_109130 crossref_primary_10_1155_2022_3451171 crossref_primary_10_1016_j_ast_2025_110056 crossref_primary_10_1109_ACCESS_2019_2960864 crossref_primary_10_1109_TAES_2022_3153761 crossref_primary_10_1155_2022_2969809 |
| Cites_doi | 10.2514/1.37030 10.1109/6979.994791 10.1016/j.ast.2017.09.030 10.2514/1.G002150 10.1007/s10514-015-9429-0 10.1016/j.ast.2018.01.033 10.2514/2.4008 10.2514/1.23034 10.2514/1.G003045 10.1016/j.ast.2017.11.009 10.1177/0954410015609361 10.2514/1.A34102 10.2514/1.A32949 10.1016/j.ast.2018.06.001 10.2514/1.A33995 10.1109/TAES.2018.2812558 10.1016/j.ast.2015.12.021 10.1016/j.ast.2018.01.040 10.1007/s10957-015-0831-8 10.1109/TITS.2010.2061971 10.2514/2.4943 10.2514/1.A33905 10.2514/1.32354 10.2514/3.20819 10.1109/TCST.2012.2237346 10.1016/j.ast.2017.05.009 10.2514/3.28504 10.2514/1.27553 10.2514/1.47202 10.1016/j.ast.2010.04.005 10.2514/1.52136 10.2514/1.58436 10.2514/1.G001210 10.1002/rnc.683 10.1016/j.ast.2015.09.008 10.2514/2.3384 10.2514/1.G002170 10.2514/1.A33566 10.1145/2558904 |
| ContentType | Journal Article |
| Copyright | 2019 Elsevier Masson SAS |
| Copyright_xml | – notice: 2019 Elsevier Masson SAS |
| DBID | AAYXX CITATION |
| DOI | 10.1016/j.ast.2019.03.002 |
| DatabaseName | CrossRef |
| DatabaseTitle | CrossRef |
| DatabaseTitleList | |
| DeliveryMethod | fulltext_linktorsrc |
| Discipline | Engineering |
| EISSN | 1626-3219 |
| EndPage | 368 |
| ExternalDocumentID | 10_1016_j_ast_2019_03_002 S1270963818317668 |
| GroupedDBID | --K --M .~1 0R~ 1B1 1~. 1~5 23M 4.4 457 4G. 5GY 5VS 7-5 71M 8P~ AACTN AAEDT AAEDW AAIAV AAIKJ AAKOC AALRI AAOAW AAQFI AAXUO ABJNI ABMAC ABXDB ABYKQ ACDAQ ACGFS ACNNM ACRLP ADBBV ADEZE ADTZH AEBSH AECPX AEKER AENEX AFKWA AFTJW AGHFR AGUBO AGYEJ AHJVU AHPGS AI. AIEXJ AIKHN AITUG AJBFU AJOXV ALMA_UNASSIGNED_HOLDINGS AMFUW AMRAJ ASPBG AVWKF AXJTR AZFZN BJAXD BKOJK BLXMC CS3 EBS EFJIC EFLBG EJD EO8 EO9 EP2 EP3 FDB FEDTE FGOYB FIRID FNPLU FYGXN G-Q GBLVA HVGLF HZ~ IHE J1W JJJVA KOM M41 MO0 N9A O-L O9- OAUVE OZT P-8 P-9 P2P PC. Q38 R2- RIG ROL RPZ SDF SDG SDP SES SEW SPC SPCBC SST SSZ T5K T9H VH1 XPP ZMT ~G- 9DU AATTM AAXKI AAYWO AAYXX ACLOT ACVFH ADCNI AEIPS AEUPX AFJKZ AFPUW AIGII AIIUN AKBMS AKRWK AKYEP ANKPU APXCP CITATION EFKBS ~HD |
| ID | FETCH-LOGICAL-c297t-95ad22e814294a5b9d38f8e5b327b5e5ebca40abfe1db5dafa28e60ad6630a643 |
| ISICitedReferencesCount | 63 |
| ISICitedReferencesURI | http://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=Summon&SrcAuth=ProQuest&DestLinkType=CitingArticles&DestApp=WOS_CPL&KeyUT=000463689000031&url=https%3A%2F%2Fcvtisr.summon.serialssolutions.com%2F%23%21%2Fsearch%3Fho%3Df%26include.ft.matches%3Dt%26l%3Dnull%26q%3D |
| ISSN | 1270-9638 |
| IngestDate | Sat Nov 29 02:08:02 EST 2025 Tue Nov 18 22:36:29 EST 2025 Fri Feb 23 02:33:24 EST 2024 |
| IsPeerReviewed | true |
| IsScholarly | true |
| Keywords | Sequential convex programming Convex optimization Mixed-integer programming Hypersonic vehicles Trajectory optimization |
| Language | English |
| LinkModel | OpenURL |
| MergedId | FETCHMERGED-LOGICAL-c297t-95ad22e814294a5b9d38f8e5b327b5e5ebca40abfe1db5dafa28e60ad6630a643 |
| ORCID | 0000-0002-8979-9765 |
| PageCount | 12 |
| ParticipantIDs | crossref_primary_10_1016_j_ast_2019_03_002 crossref_citationtrail_10_1016_j_ast_2019_03_002 elsevier_sciencedirect_doi_10_1016_j_ast_2019_03_002 |
| PublicationCentury | 2000 |
| PublicationDate | April 2019 2019-04-00 |
| PublicationDateYYYYMMDD | 2019-04-01 |
| PublicationDate_xml | – month: 04 year: 2019 text: April 2019 |
| PublicationDecade | 2010 |
| PublicationTitle | Aerospace science and technology |
| PublicationYear | 2019 |
| Publisher | Elsevier Masson SAS |
| Publisher_xml | – name: Elsevier Masson SAS |
| References | Wang, Grant (br0420) 2018; 55 Windhorst, Ardema, Bowles (br0080) 1998; 35 She, Li, Zhao (br0230) 2018; 72 Betts, Huffman (br0040) 1992; 15 Rao, Clarke (br0150) August 2002 Wang, Grant (br0480) 2017; 40 Pallottino, Feron, Bicchi (br0240) 2002; 3 Acikmese, Ploen (br0320) 2007; 30 Mao, Szmuk, Acikmese (br0530) 2016 Pinson, Lu (br0390) 2018; 41 Gurobi Optimization, Inc. (br0570) 2018 Sagliano, Mooij (br0490) 2018 Liu, Lu (br0370) 2013 Liu, Shen, Lu (br0450) 2016; 39 Dirkx, Mooij (br0190) 2017 Kamal, Gu, Postlethwaite (br0260) December 2005 Wang (br0500) 2019 Li, Hu, Ding, Liu, He (br0160) 2018; 76 Yang, Bai, Baoyin (br0380) 2017; 40 Liu, Shen (br0470) 2016; 168 Liu, Shen, Lu (br0460) 2015; 47 Darby, Hager, Rao (br0050) 2011; 48 Liu (br0350) 2017 Gallais (br0010) 2007 Radmanesh, Kumar (br0270) 2016; 50 Domahidi, Chu, Boyd (br0550) 2013 Blackmore, Acikmese, Scharf (br0330) 2010; 33 Szmuk, Acikmese, Berning (br0520) 2016 Lafleur, Cerimele (br0130) August 2008 Chen, Ho (br0220) 2018; 55 Wu, Cao, Xing, Zheng, Zhang (br0410) 2010; 14 Zhang, Li, Wang (br0310) 2018; 76 Grant, Braun (br0090) 2015; 52 Szmuk, Eren, Acikmese (br0540) 2017 Acikmese, Carson, Blackmore (br0340) 2013; 21 Augugliaro, Schoellig, D'Andrea (br0290) October 2012 Jiang, An, Yu, Chen, Xiong (br0440) 2018; 79 Istratie (br0120) June 2008 Lu, Liu (br0360) 2013; 36 Richards, Schouwenaars, How, Feron (br0210) 2002; 25 Viviani, Iuspa, Aprovitola (br0170) 2017; 68 Alonso-Ayuso, Escudero, Martin-Campo (br0250) 2002; 12 Leavitt, Mease (br0060) 2007; 30 Zheng, Cui, Ai (br0140) 2017; 54 Viviani, Iuspa, Aprovitola (br0180) 2017; 71 Schouwenaars, De Moor, Feron, How (br0200) September 2001 Tillerson, Inalhan, How (br0400) 2002; 12 Jorris, Cobb (br0100) 2008; 31 Wang, Grant (br0430) 2018; 54 Patterson, Rao (br0560) 2014; 41 Jorris, Cobb (br0110) 2008; 32 Leondes, Miemann (br0020) 1966; 3 Wang, Grant (br0510) 2018; 55 Radmanesh, Kumar, Nemati, Sarim (br0280) 2016; 230 Lu (br0070) 1997; 20 Tava, Suzuki (br0030) 2001 Alonso-Mora, Naegeli, Siegwart, Beardsley (br0300) 2015; 39 Wu (10.1016/j.ast.2019.03.002_br0410) 2010; 14 Gallais (10.1016/j.ast.2019.03.002_br0010) 2007 Liu (10.1016/j.ast.2019.03.002_br0370) 2013 Kamal (10.1016/j.ast.2019.03.002_br0260) 2005 Wang (10.1016/j.ast.2019.03.002_br0430) 2018; 54 Liu (10.1016/j.ast.2019.03.002_br0450) 2016; 39 Li (10.1016/j.ast.2019.03.002_br0160) 2018; 76 Windhorst (10.1016/j.ast.2019.03.002_br0080) 1998; 35 Sagliano (10.1016/j.ast.2019.03.002_br0490) 2018 Leavitt (10.1016/j.ast.2019.03.002_br0060) 2007; 30 Radmanesh (10.1016/j.ast.2019.03.002_br0270) 2016; 50 Yang (10.1016/j.ast.2019.03.002_br0380) 2017; 40 Pallottino (10.1016/j.ast.2019.03.002_br0240) 2002; 3 Radmanesh (10.1016/j.ast.2019.03.002_br0280) 2016; 230 Chen (10.1016/j.ast.2019.03.002_br0220) 2018; 55 Mao (10.1016/j.ast.2019.03.002_br0530) 2016 Viviani (10.1016/j.ast.2019.03.002_br0180) 2017; 71 Schouwenaars (10.1016/j.ast.2019.03.002_br0200) 2001 Wang (10.1016/j.ast.2019.03.002_br0510) 2018; 55 Tava (10.1016/j.ast.2019.03.002_br0030) 2001 Augugliaro (10.1016/j.ast.2019.03.002_br0290) 2012 Grant (10.1016/j.ast.2019.03.002_br0090) 2015; 52 Jiang (10.1016/j.ast.2019.03.002_br0440) 2018; 79 Rao (10.1016/j.ast.2019.03.002_br0150) 2002 Jorris (10.1016/j.ast.2019.03.002_br0100) 2008; 31 Pinson (10.1016/j.ast.2019.03.002_br0390) 2018; 41 Viviani (10.1016/j.ast.2019.03.002_br0170) 2017; 68 Acikmese (10.1016/j.ast.2019.03.002_br0340) 2013; 21 Patterson (10.1016/j.ast.2019.03.002_br0560) 2014; 41 Liu (10.1016/j.ast.2019.03.002_br0470) 2016; 168 Acikmese (10.1016/j.ast.2019.03.002_br0320) 2007; 30 Liu (10.1016/j.ast.2019.03.002_br0460) 2015; 47 Lu (10.1016/j.ast.2019.03.002_br0070) 1997; 20 Jorris (10.1016/j.ast.2019.03.002_br0110) 2008; 32 Liu (10.1016/j.ast.2019.03.002_br0350) 2017 Darby (10.1016/j.ast.2019.03.002_br0050) 2011; 48 She (10.1016/j.ast.2019.03.002_br0230) 2018; 72 Gurobi Optimization, Inc. (10.1016/j.ast.2019.03.002_br0570) Domahidi (10.1016/j.ast.2019.03.002_br0550) 2013 Wang (10.1016/j.ast.2019.03.002_br0480) 2017; 40 Alonso-Mora (10.1016/j.ast.2019.03.002_br0300) 2015; 39 Zhang (10.1016/j.ast.2019.03.002_br0310) 2018; 76 Wang (10.1016/j.ast.2019.03.002_br0500) 2019 Lu (10.1016/j.ast.2019.03.002_br0360) 2013; 36 Zheng (10.1016/j.ast.2019.03.002_br0140) 2017; 54 Wang (10.1016/j.ast.2019.03.002_br0420) 2018; 55 Blackmore (10.1016/j.ast.2019.03.002_br0330) 2010; 33 Szmuk (10.1016/j.ast.2019.03.002_br0520) 2016 Szmuk (10.1016/j.ast.2019.03.002_br0540) 2017 Leondes (10.1016/j.ast.2019.03.002_br0020) 1966; 3 Betts (10.1016/j.ast.2019.03.002_br0040) 1992; 15 Dirkx (10.1016/j.ast.2019.03.002_br0190) 2017 Istratie (10.1016/j.ast.2019.03.002_br0120) 2008 Alonso-Ayuso (10.1016/j.ast.2019.03.002_br0250) 2002; 12 Richards (10.1016/j.ast.2019.03.002_br0210) 2002; 25 Lafleur (10.1016/j.ast.2019.03.002_br0130) 2008 Tillerson (10.1016/j.ast.2019.03.002_br0400) 2002; 12 |
| References_xml | – volume: 41 start-page: 1243 year: 2018 end-page: 1256 ident: br0390 article-title: Trajectory design employing convex optimization for landing on irregularly shaped asteroids publication-title: J. Guid. Control Dyn. – volume: 79 start-page: 426 year: 2018 end-page: 440 ident: br0440 article-title: Cooperative guidance with multiple constraints using convex optimization publication-title: Aerosp. Sci. Technol. – start-page: 3071 year: 2013 end-page: 3076 ident: br0550 article-title: ECOS: an SOCP solver for embedded system publication-title: European Control Conference – year: 2017 ident: br0350 article-title: Fuel-optimal rocket landing with aerodynamic controls publication-title: AIAA Guidance, Navigation, and Control Conference – year: October 2012 ident: br0290 article-title: Generation of collision-free trajectories for a quadrocopter fleet: a sequential convex programming approach publication-title: IEEE/RSJ International Conference on Intelligent Robots and Systems – volume: 20 start-page: 143 year: 1997 end-page: 149 ident: br0070 article-title: Entry guidance and trajectory control for reusable launch vehicle publication-title: J. Guid. Control Dyn. – volume: 52 start-page: 177 year: 2015 end-page: 182 ident: br0090 article-title: Rapid indirect trajectory optimization for conceptual design of hypersonic missions publication-title: J. Spacecr. Rockets – volume: 40 start-page: 628 year: 2017 end-page: 641 ident: br0380 article-title: Rapid generation of time-optimal trajectories for asteroid landing via convex optimization publication-title: J. Guid. Control Dyn. – year: 2019 ident: br0500 article-title: Maximum-normal-load entry trajectory optimization for hypersonic glide vehicles publication-title: AIAA Atmospheric Flight Mechanics Conference – volume: 3 start-page: 618 year: 1966 end-page: 623 ident: br0020 article-title: Optimization of aerospace re-entry vehicle trajectories through independent control of lift and drag publication-title: J. Spacecr. Rockets – volume: 3 start-page: 3 year: 2002 end-page: 11 ident: br0240 article-title: Conflict resolution problems for air traffic management systems solved with mixed integer programming publication-title: IEEE Trans. Intell. Transp. Syst. – volume: 54 start-page: 2274 year: 2018 end-page: 2290 ident: br0430 article-title: Minimum-fuel low-thrust transfers for spacecraft: a convex approach publication-title: IEEE Trans. Aerosp. Electron. Syst. – volume: 47 start-page: 10 year: 2015 end-page: 20 ident: br0460 article-title: Solving the maximum-crossrange problem via successive second-order cone programming with a line search publication-title: Aerosp. Sci. Technol. – volume: 39 start-page: 101 year: 2015 end-page: 121 ident: br0300 article-title: Collision avoidance for aerial vehicles in multi-agent scenarios publication-title: Auton. Robots – volume: 76 start-page: 280 year: 2018 end-page: 290 ident: br0310 article-title: Sequential convex programming for nonlinear optimal control problems in UAV path planning publication-title: Aerosp. Sci. Technol. – year: 2017 ident: br0540 article-title: Successive convexification for Mars 6-DoF powered descent landing guidance publication-title: AIAA Guidance, Navigation, and Control Conference – volume: 14 start-page: 415 year: 2010 end-page: 428 ident: br0410 article-title: Relative motion coupled control for formation flying spacecraft via convex optimization publication-title: Aerosp. Sci. Technol. – year: August 2008 ident: br0130 article-title: Mars entry bank profile design for terminal state optimization publication-title: AIAA Atmospheric Flight Mechanics Conference and Exhibit – volume: 76 start-page: 176 year: 2018 end-page: 186 ident: br0160 article-title: Stochastic gradient particle swarm optimization based entry trajectory rapid planning for hypersonic glide vehicles publication-title: Aerosp. Sci. Technol. – volume: 68 start-page: 123 year: 2017 end-page: 134 ident: br0170 article-title: An optimization-based procedure for self-generation of re-entry vehicles shape publication-title: Aerosp. Sci. Technol. – volume: 40 start-page: 2603 year: 2017 end-page: 2615 ident: br0480 article-title: Constrained trajectory optimization for planetary entry via sequential convex programming publication-title: J. Guid. Control Dyn. – volume: 48 start-page: 433 year: 2011 end-page: 445 ident: br0050 article-title: Direct trajectory optimization using a variable low-order adaptive pseudospectral method publication-title: J. Spacecr. Rockets – year: 2013 ident: br0370 article-title: Robust trajectory optimization for highly constrained rendezvous and proximity operations publication-title: AIAA Guidance, Navigation, and Control Conference – year: June 2008 ident: br0120 article-title: Optimal skip entry with terminal maximum velocity and heat constraint publication-title: AIAA/ASME Joint Thermophysics and Heat Transfer Conference – volume: 25 start-page: 755 year: 2002 end-page: 764 ident: br0210 article-title: Spacecraft trajectory planning with avoidance constraints using mixed-integer linear programming publication-title: J. Guid. Control Dyn. – volume: 12 start-page: 47 year: 2002 end-page: 57 ident: br0250 article-title: Collision avoidance in air traffic management: a mixed-integer linear optimization approach publication-title: IEEE Trans. Intell. Transp. Syst. – volume: 72 start-page: 204 year: 2018 end-page: 216 ident: br0230 article-title: Onboard mission planning for agile satellite using modified mixed-integer linear programming publication-title: Aerosp. Sci. Technol. – volume: 12 start-page: 207 year: 2002 end-page: 242 ident: br0400 article-title: Co-ordination and control of distributed spacecraft systems using convex optimization techniques publication-title: Int. J. Robust Nonlinear Control – volume: 230 start-page: 1668 year: 2016 end-page: 1682 ident: br0280 article-title: Dynamic optimal UAV trajectory planning in the national airspace system via mixed integer linear programming publication-title: Proc. Inst. Mech. Eng., Part G, J. Aerosp. Eng. – volume: 30 start-page: 1353 year: 2007 end-page: 1366 ident: br0320 article-title: Convex programming approach to powered descent guidance for Mars landing publication-title: J. Guid. Control Dyn. – volume: 32 start-page: 551 year: 2008 end-page: 572 ident: br0110 article-title: Three-dimensional trajectory optimization satisfying waypoint and no-fly zone constraints publication-title: J. Guid. Control Dyn. – volume: 71 start-page: 312 year: 2017 end-page: 324 ident: br0180 article-title: Multi-objective optimization for re-entry spacecraft conceptual design using a free-form shape generator publication-title: Aerosp. Sci. Technol. – year: 2018 ident: br0490 article-title: Optimal drag-energy entry guidance via pseudospectral convex optimization publication-title: AIAA Guidance, Navigation, and Control Conference – volume: 35 start-page: 672 year: 1998 end-page: 682 ident: br0080 article-title: Minimum heating entry trajectories for reusable launch vehicles publication-title: J. Spacecr. Rockets – volume: 54 start-page: 1068 year: 2017 end-page: 1080 ident: br0140 article-title: Indirect trajectory optimization for Mars entry with maximum terminal altitude publication-title: J. Spacecr. Rockets – year: 2017 ident: br0190 article-title: Conceptual shape optimization of entry vehicles: applied to capsules and winged fuselage vehicles publication-title: Springer Aerospace Technology – volume: 33 start-page: 1161 year: 2010 end-page: 1171 ident: br0330 article-title: Minimum landing error powered descent guidance for Mars landing using convex optimization publication-title: J. Guid. Control Dyn. – volume: 55 start-page: 365 year: 2018 end-page: 381 ident: br0220 article-title: Integrated space logistics mission planning and spacecraft design with mixed-integer nonlinear programming publication-title: J. Spacecr. Rockets – volume: 39 start-page: 227 year: 2016 end-page: 241 ident: br0450 article-title: Entry trajectory optimization by second-order cone programming publication-title: J. Guid. Control Dyn. – year: September 2001 ident: br0200 article-title: Mixed integer programming for multi-vehicle path-planning publication-title: European Control Conference – volume: 36 start-page: 375 year: 2013 end-page: 389 ident: br0360 article-title: Autonomous trajectory planning for rendezvous and proximity operations by conic optimization publication-title: J. Guid. Control Dyn. – year: 2018 ident: br0570 article-title: Gurobi optimizer reference manual – volume: 55 start-page: 586 year: 2018 end-page: 598 ident: br0420 article-title: Optimization of minimum-time low-thrust transfers using convex programming publication-title: J. Spacecr. Rockets – volume: 41 start-page: 1 year: 2014 end-page: 37 ident: br0560 article-title: Gpops-II: a MATLAB software for solving multiple-phase optimal control problems using hp-adaptive Gaussian quadrature collocation methods and sparse nonlinear programming publication-title: ACM Trans. Math. Softw. – volume: 15 start-page: 198 year: 1992 end-page: 206 ident: br0040 article-title: Application of sparse nonlinear programming to trajectory optimization publication-title: J. Guid. Control Dyn. – volume: 21 start-page: 2104 year: 2013 end-page: 2113 ident: br0340 article-title: Lossless convexification of nonconvex control bound and pointing constraints of the soft landing optimal control problem publication-title: IEEE Trans. Control Syst. Technol. – year: 2001 ident: br0030 article-title: Multidisciplinary Design Optimization of a Re-Entry Vehicle Shape and Trajectory – volume: 55 start-page: 993 year: 2018 end-page: 1006 ident: br0510 article-title: Autonomous entry guidance for hypersonic vehicles by convex optimization publication-title: J. Spacecr. Rockets – year: 2007 ident: br0010 article-title: Atmospheric Re-Entry Vehicle Mechanics – volume: 50 start-page: 149 year: 2016 end-page: 160 ident: br0270 article-title: Flight formation of UAVs in presence of moving obstacles using fast-dynamic mixed integer linear programming publication-title: Aerosp. Sci. Technol. – year: 2016 ident: br0520 article-title: Successive convexification for fuel-optimal powered landing with aerodynamic drag and non-convex constraints publication-title: AIAA Guidance, Navigation, and Control Conference – volume: 168 start-page: 917 year: 2016 end-page: 943 ident: br0470 article-title: Rapid smooth entry trajectory planning for high lift/drag hypersonic glide vehicles publication-title: J. Optim. Theory Appl. – year: August 2002 ident: br0150 article-title: Performance optimization of a maneuvering re-entry vehicle using a Legendre pseudospectral method publication-title: AIAA Atmospheric Flight Mechanics Conference and Exhibit – volume: 31 start-page: 543 year: 2008 end-page: 553 ident: br0100 article-title: Multiple method 2-D trajectory optimization satisfying waypoints and no-fly zone constraints publication-title: J. Guid. Control Dyn. – volume: 30 start-page: 473 year: 2007 end-page: 481 ident: br0060 article-title: Feasible trajectory generation for atmospheric entry guidance publication-title: J. Guid. Control Dyn. – year: December 2005 ident: br0260 article-title: Real time trajectory planning for UAVs using MILP publication-title: IEEE Conference on Decision and Control and European Control Conference – year: 2016 ident: br0530 article-title: Successive convexification of non-convex optimal control problems and its convergence properties publication-title: IEEE Conference on Decision and Control, las Vegas – year: 2008 ident: 10.1016/j.ast.2019.03.002_br0130 article-title: Mars entry bank profile design for terminal state optimization – volume: 32 start-page: 551 issue: 2 year: 2008 ident: 10.1016/j.ast.2019.03.002_br0110 article-title: Three-dimensional trajectory optimization satisfying waypoint and no-fly zone constraints publication-title: J. Guid. Control Dyn. doi: 10.2514/1.37030 – volume: 3 start-page: 3 issue: 1 year: 2002 ident: 10.1016/j.ast.2019.03.002_br0240 article-title: Conflict resolution problems for air traffic management systems solved with mixed integer programming publication-title: IEEE Trans. Intell. Transp. Syst. doi: 10.1109/6979.994791 – volume: 71 start-page: 312 year: 2017 ident: 10.1016/j.ast.2019.03.002_br0180 article-title: Multi-objective optimization for re-entry spacecraft conceptual design using a free-form shape generator publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2017.09.030 – volume: 40 start-page: 2603 issue: 10 year: 2017 ident: 10.1016/j.ast.2019.03.002_br0480 article-title: Constrained trajectory optimization for planetary entry via sequential convex programming publication-title: J. Guid. Control Dyn. doi: 10.2514/1.G002150 – volume: 39 start-page: 101 issue: 1 year: 2015 ident: 10.1016/j.ast.2019.03.002_br0300 article-title: Collision avoidance for aerial vehicles in multi-agent scenarios publication-title: Auton. Robots doi: 10.1007/s10514-015-9429-0 – year: 2007 ident: 10.1016/j.ast.2019.03.002_br0010 – year: 2001 ident: 10.1016/j.ast.2019.03.002_br0200 article-title: Mixed integer programming for multi-vehicle path-planning – volume: 76 start-page: 176 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0160 article-title: Stochastic gradient particle swarm optimization based entry trajectory rapid planning for hypersonic glide vehicles publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.01.033 – volume: 20 start-page: 143 issue: 1 year: 1997 ident: 10.1016/j.ast.2019.03.002_br0070 article-title: Entry guidance and trajectory control for reusable launch vehicle publication-title: J. Guid. Control Dyn. doi: 10.2514/2.4008 – volume: 30 start-page: 473 issue: 2 year: 2007 ident: 10.1016/j.ast.2019.03.002_br0060 article-title: Feasible trajectory generation for atmospheric entry guidance publication-title: J. Guid. Control Dyn. doi: 10.2514/1.23034 – volume: 41 start-page: 1243 issue: 6 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0390 article-title: Trajectory design employing convex optimization for landing on irregularly shaped asteroids publication-title: J. Guid. Control Dyn. doi: 10.2514/1.G003045 – year: 2017 ident: 10.1016/j.ast.2019.03.002_br0190 article-title: Conceptual shape optimization of entry vehicles: applied to capsules and winged fuselage vehicles – year: 2017 ident: 10.1016/j.ast.2019.03.002_br0350 article-title: Fuel-optimal rocket landing with aerodynamic controls – year: 2018 ident: 10.1016/j.ast.2019.03.002_br0490 article-title: Optimal drag-energy entry guidance via pseudospectral convex optimization – volume: 72 start-page: 204 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0230 article-title: Onboard mission planning for agile satellite using modified mixed-integer linear programming publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2017.11.009 – volume: 230 start-page: 1668 issue: 9 year: 2016 ident: 10.1016/j.ast.2019.03.002_br0280 article-title: Dynamic optimal UAV trajectory planning in the national airspace system via mixed integer linear programming publication-title: Proc. Inst. Mech. Eng., Part G, J. Aerosp. Eng. doi: 10.1177/0954410015609361 – year: 2012 ident: 10.1016/j.ast.2019.03.002_br0290 article-title: Generation of collision-free trajectories for a quadrocopter fleet: a sequential convex programming approach – volume: 55 start-page: 993 issue: 4 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0510 article-title: Autonomous entry guidance for hypersonic vehicles by convex optimization publication-title: J. Spacecr. Rockets doi: 10.2514/1.A34102 – volume: 52 start-page: 177 issue: 1 year: 2015 ident: 10.1016/j.ast.2019.03.002_br0090 article-title: Rapid indirect trajectory optimization for conceptual design of hypersonic missions publication-title: J. Spacecr. Rockets doi: 10.2514/1.A32949 – volume: 79 start-page: 426 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0440 article-title: Cooperative guidance with multiple constraints using convex optimization publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.06.001 – start-page: 3071 year: 2013 ident: 10.1016/j.ast.2019.03.002_br0550 article-title: ECOS: an SOCP solver for embedded system – volume: 55 start-page: 586 issue: 3 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0420 article-title: Optimization of minimum-time low-thrust transfers using convex programming publication-title: J. Spacecr. Rockets doi: 10.2514/1.A33995 – volume: 54 start-page: 2274 issue: 5 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0430 article-title: Minimum-fuel low-thrust transfers for spacecraft: a convex approach publication-title: IEEE Trans. Aerosp. Electron. Syst. doi: 10.1109/TAES.2018.2812558 – year: 2002 ident: 10.1016/j.ast.2019.03.002_br0150 article-title: Performance optimization of a maneuvering re-entry vehicle using a Legendre pseudospectral method – volume: 50 start-page: 149 year: 2016 ident: 10.1016/j.ast.2019.03.002_br0270 article-title: Flight formation of UAVs in presence of moving obstacles using fast-dynamic mixed integer linear programming publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2015.12.021 – volume: 76 start-page: 280 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0310 article-title: Sequential convex programming for nonlinear optimal control problems in UAV path planning publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.01.040 – year: 2016 ident: 10.1016/j.ast.2019.03.002_br0530 article-title: Successive convexification of non-convex optimal control problems and its convergence properties – ident: 10.1016/j.ast.2019.03.002_br0570 – volume: 168 start-page: 917 issue: 3 year: 2016 ident: 10.1016/j.ast.2019.03.002_br0470 article-title: Rapid smooth entry trajectory planning for high lift/drag hypersonic glide vehicles publication-title: J. Optim. Theory Appl. doi: 10.1007/s10957-015-0831-8 – volume: 12 start-page: 47 issue: 1 year: 2002 ident: 10.1016/j.ast.2019.03.002_br0250 article-title: Collision avoidance in air traffic management: a mixed-integer linear optimization approach publication-title: IEEE Trans. Intell. Transp. Syst. doi: 10.1109/TITS.2010.2061971 – volume: 25 start-page: 755 issue: 4 year: 2002 ident: 10.1016/j.ast.2019.03.002_br0210 article-title: Spacecraft trajectory planning with avoidance constraints using mixed-integer linear programming publication-title: J. Guid. Control Dyn. doi: 10.2514/2.4943 – volume: 55 start-page: 365 issue: 2 year: 2018 ident: 10.1016/j.ast.2019.03.002_br0220 article-title: Integrated space logistics mission planning and spacecraft design with mixed-integer nonlinear programming publication-title: J. Spacecr. Rockets doi: 10.2514/1.A33905 – volume: 31 start-page: 543 issue: 3 year: 2008 ident: 10.1016/j.ast.2019.03.002_br0100 article-title: Multiple method 2-D trajectory optimization satisfying waypoints and no-fly zone constraints publication-title: J. Guid. Control Dyn. doi: 10.2514/1.32354 – volume: 15 start-page: 198 issue: 1 year: 1992 ident: 10.1016/j.ast.2019.03.002_br0040 article-title: Application of sparse nonlinear programming to trajectory optimization publication-title: J. Guid. Control Dyn. doi: 10.2514/3.20819 – volume: 21 start-page: 2104 issue: 6 year: 2013 ident: 10.1016/j.ast.2019.03.002_br0340 article-title: Lossless convexification of nonconvex control bound and pointing constraints of the soft landing optimal control problem publication-title: IEEE Trans. Control Syst. Technol. doi: 10.1109/TCST.2012.2237346 – volume: 68 start-page: 123 year: 2017 ident: 10.1016/j.ast.2019.03.002_br0170 article-title: An optimization-based procedure for self-generation of re-entry vehicles shape publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2017.05.009 – volume: 3 start-page: 618 issue: 5 year: 1966 ident: 10.1016/j.ast.2019.03.002_br0020 article-title: Optimization of aerospace re-entry vehicle trajectories through independent control of lift and drag publication-title: J. Spacecr. Rockets doi: 10.2514/3.28504 – volume: 30 start-page: 1353 issue: 5 year: 2007 ident: 10.1016/j.ast.2019.03.002_br0320 article-title: Convex programming approach to powered descent guidance for Mars landing publication-title: J. Guid. Control Dyn. doi: 10.2514/1.27553 – year: 2017 ident: 10.1016/j.ast.2019.03.002_br0540 article-title: Successive convexification for Mars 6-DoF powered descent landing guidance – volume: 33 start-page: 1161 issue: 4 year: 2010 ident: 10.1016/j.ast.2019.03.002_br0330 article-title: Minimum landing error powered descent guidance for Mars landing using convex optimization publication-title: J. Guid. Control Dyn. doi: 10.2514/1.47202 – year: 2016 ident: 10.1016/j.ast.2019.03.002_br0520 article-title: Successive convexification for fuel-optimal powered landing with aerodynamic drag and non-convex constraints – volume: 14 start-page: 415 issue: 6 year: 2010 ident: 10.1016/j.ast.2019.03.002_br0410 article-title: Relative motion coupled control for formation flying spacecraft via convex optimization publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2010.04.005 – volume: 48 start-page: 433 issue: 3 year: 2011 ident: 10.1016/j.ast.2019.03.002_br0050 article-title: Direct trajectory optimization using a variable low-order adaptive pseudospectral method publication-title: J. Spacecr. Rockets doi: 10.2514/1.52136 – volume: 36 start-page: 375 issue: 2 year: 2013 ident: 10.1016/j.ast.2019.03.002_br0360 article-title: Autonomous trajectory planning for rendezvous and proximity operations by conic optimization publication-title: J. Guid. Control Dyn. doi: 10.2514/1.58436 – year: 2001 ident: 10.1016/j.ast.2019.03.002_br0030 – year: 2013 ident: 10.1016/j.ast.2019.03.002_br0370 article-title: Robust trajectory optimization for highly constrained rendezvous and proximity operations – volume: 39 start-page: 227 issue: 2 year: 2016 ident: 10.1016/j.ast.2019.03.002_br0450 article-title: Entry trajectory optimization by second-order cone programming publication-title: J. Guid. Control Dyn. doi: 10.2514/1.G001210 – volume: 12 start-page: 207 issue: 2–3 year: 2002 ident: 10.1016/j.ast.2019.03.002_br0400 article-title: Co-ordination and control of distributed spacecraft systems using convex optimization techniques publication-title: Int. J. Robust Nonlinear Control doi: 10.1002/rnc.683 – volume: 47 start-page: 10 year: 2015 ident: 10.1016/j.ast.2019.03.002_br0460 article-title: Solving the maximum-crossrange problem via successive second-order cone programming with a line search publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2015.09.008 – volume: 35 start-page: 672 issue: 5 year: 1998 ident: 10.1016/j.ast.2019.03.002_br0080 article-title: Minimum heating entry trajectories for reusable launch vehicles publication-title: J. Spacecr. Rockets doi: 10.2514/2.3384 – volume: 40 start-page: 628 issue: 3 year: 2017 ident: 10.1016/j.ast.2019.03.002_br0380 article-title: Rapid generation of time-optimal trajectories for asteroid landing via convex optimization publication-title: J. Guid. Control Dyn. doi: 10.2514/1.G002170 – year: 2008 ident: 10.1016/j.ast.2019.03.002_br0120 article-title: Optimal skip entry with terminal maximum velocity and heat constraint – volume: 54 start-page: 1068 issue: 5 year: 2017 ident: 10.1016/j.ast.2019.03.002_br0140 article-title: Indirect trajectory optimization for Mars entry with maximum terminal altitude publication-title: J. Spacecr. Rockets doi: 10.2514/1.A33566 – year: 2019 ident: 10.1016/j.ast.2019.03.002_br0500 article-title: Maximum-normal-load entry trajectory optimization for hypersonic glide vehicles – year: 2005 ident: 10.1016/j.ast.2019.03.002_br0260 article-title: Real time trajectory planning for UAVs using MILP – volume: 41 start-page: 1 issue: 1 year: 2014 ident: 10.1016/j.ast.2019.03.002_br0560 article-title: Gpops-II: a MATLAB software for solving multiple-phase optimal control problems using hp-adaptive Gaussian quadrature collocation methods and sparse nonlinear programming publication-title: ACM Trans. Math. Softw. doi: 10.1145/2558904 |
| SSID | ssj0002942 |
| Score | 2.4477174 |
| Snippet | Hypersonic trajectory optimization has been intensively investigated through different approaches; however, the normal-load-optimal entry problems were barely... |
| SourceID | crossref elsevier |
| SourceType | Enrichment Source Index Database Publisher |
| StartPage | 357 |
| SubjectTerms | Convex optimization Hypersonic vehicles Mixed-integer programming Sequential convex programming Trajectory optimization |
| Title | Optimal trajectories and normal load analysis of hypersonic glide vehicles via convex optimization |
| URI | https://dx.doi.org/10.1016/j.ast.2019.03.002 |
| Volume | 87 |
| WOSCitedRecordID | wos000463689000031&url=https%3A%2F%2Fcvtisr.summon.serialssolutions.com%2F%23%21%2Fsearch%3Fho%3Df%26include.ft.matches%3Dt%26l%3Dnull%26q%3D |
| hasFullText | 1 |
| inHoldings | 1 |
| isFullTextHit | |
| isPrint | |
| journalDatabaseRights | – providerCode: PRVESC databaseName: Elsevier SD Freedom Collection Journals 2021 customDbUrl: eissn: 1626-3219 dateEnd: 99991231 omitProxy: false ssIdentifier: ssj0002942 issn: 1270-9638 databaseCode: AIEXJ dateStart: 19970101 isFulltext: true titleUrlDefault: https://www.sciencedirect.com providerName: Elsevier |
| link | http://cvtisr.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwtZ3PT9swFMetCThsB7TBpgFj8mGnRZkcO5ntYzWBAE1sBzZVXCI7dkarLkG0VP3z9_wjacRggsMuURQ1bpqP-96z_fV7CH1gzOS81ipl2rA0V3WRaiJMKmVFqAb_XPl0TT-_8vNzMR7L77Ha6NyXE-BNI1Yref1fUcM1gO22zj4Bd98oXIBzgA5HwA7HR4H_Bkbgt5eQq6mfkoexsF8iaFx4OktmrXLpWde5SK5gKOrC7kmV_JpNjE2W9sqL5ZLlRAVZ-ippXatxz-YwoB1ZcLMw7rZJt0HISzLvmbAPRuXSScra4VxDJgcSlWAeKSep-8sO7Wd0mMEAspBuOvpSFkrm_GWmw4zB9JOaOzlrFvPM0rVP6tbh77iqXkDYadOmJTRRuiZKwkqfVXST8kKCfdscnR6Nz3qvTKUvpNT_gm6F22v97jzH_THKIO64eIm244ABjwLoV-iZbXbQi0EayV2kI3I8RI6BAw7IsUOOO-S4rfEaOfbIcYccA3IckOMh8tfox_HRxZeTNNbOSCsq-SKVhTKUWpFBvJGrQkvDRC1soRnlurCF08DlROnaZkYXRtWKCvuZKAMRKFEQpr5BG03b2LcI80xaSmsjIK7JtRuQslwoTjLFNDWV2kOke1tlFRPLu_oms_JBSnvoY3_Ldciq8q8P5x2CMnblEO6V0J0evm3_Kd9xgJ6v-_s7tLG4ubWHaKtaLibzm_exL_0BnPKHiA |
| linkProvider | Elsevier |
| openUrl | ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Optimal+trajectories+and+normal+load+analysis+of+hypersonic+glide+vehicles+via+convex+optimization&rft.jtitle=Aerospace+science+and+technology&rft.au=Wang%2C+Zhenbo&rft.date=2019-04-01&rft.issn=1270-9638&rft.volume=87&rft.spage=357&rft.epage=368&rft_id=info:doi/10.1016%2Fj.ast.2019.03.002&rft.externalDBID=n%2Fa&rft.externalDocID=10_1016_j_ast_2019_03_002 |
| thumbnail_l | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1270-9638&client=summon |
| thumbnail_m | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1270-9638&client=summon |
| thumbnail_s | http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1270-9638&client=summon |