Suchergebnisse - Guidance and Trajectory Optimization Algorithms

  1. 1

    Online trajectory optimization and guidance algorithm for space interceptors with nonlinear terminal constraints via convex programming von Li, Yuan, Sun, Ruisheng, Chen, Wei

    ISSN: 1748-8842, 1758-4213, 1748-8842
    Veröffentlicht: Bradford Emerald Publishing Limited 02.01.2023
    Veröffentlicht in Aircraft engineering (02.01.2023)
    “… Purpose In this paper, an online convex optimization method for the exoatmospheric ascent trajectory of space interceptors is proposed …”
    Volltext
    Journal Article
  2. 2

    Ascent Guidance Trajectory Optimization Using Evolutionary Algorithm Considering Engine Gimbal and Aerodynamic Control von Murakami, Masaaki, Yonemoto, Koichi, Fujikawa, Takahiro

    ISSN: 2093-274X, 2093-2480
    Veröffentlicht: Seoul The Korean Society for Aeronautical & Space Sciences (KSAS) 01.09.2022
    “… The application of an evolutionary algorithm to the real-time optimization of longitudinal ascent guidance trajectories is presented herein …”
    Volltext
    Journal Article
  3. 3

    Re-Entry Trajectory Design with Use of Aided Optimization Algorithm through Combination of Classic Guidance Acceleration Profile Optimization von Mohammad Javad Poustini, Seyed Hossein Sadati, Yosof Abbasi, Seyyed Majid Hosseini

    ISSN: 2008-4560, 2423-4516
    Veröffentlicht: Aerospace Research Institute 01.03.2022
    Veröffentlicht in فصلنامه علوم و فناوری فضایی (01.03.2022)
    “… Trajectory optimization is a familiar method for most of re-entry and Re-usable vehicles …”
    Volltext
    Journal Article
  4. 4

    Interval Estimation of Motion Intensity Variation Using the Improved Inception-V3 Model von Wang, Wendong, Li, Hanhao, Zhao, Chengzhi, Kong, Dezhi, Zhang, Peng

    ISSN: 2169-3536, 2169-3536
    Veröffentlicht: Piscataway IEEE 2021
    Veröffentlicht in IEEE access (2021)
    “… Finally, the manipulator's trajectory optimization …”
    Volltext
    Journal Article
  5. 5

    Improving Entry Vehicle Shape Optimization via a Guidance Algorithm for Trajectory Generation von D'Souza, Sarah Nicole

    ISBN: 1303538091, 9781303538094
    Veröffentlicht: ProQuest Dissertations & Theses 01.01.2013
    “… In order to address a gap in modeling flight feasible trajectories for vehicle shape optimization, a novel guidance algorithm was developed for this application …”
    Volltext
    Dissertation
  6. 6

    Recovery trajectory planning for the reusable launch vehicle von Cheng, Guanghui, Jing, Wuxing, Gao, Changsheng

    ISSN: 1270-9638, 1626-3219
    Veröffentlicht: Elsevier Masson SAS 01.10.2021
    Veröffentlicht in Aerospace science and technology (01.10.2021)
    “… Secondly, a compound trajectory planning method, which combines Particle Swarm Optimization algorithm (PSO …”
    Volltext
    Journal Article
  7. 7

    A Trajectory Generation Algorithm for a Re-Entry Gliding Vehicle Based on Convex Optimization in the Flight Range Domain and Distributed Grid Points Adjustment von Li, Mingjie, Zhou, Chijun, Shao, Lei, Lei, Humin, Luo, Changxin

    ISSN: 2076-3417, 2076-3417
    Veröffentlicht: Basel MDPI AG 01.02.2023
    Veröffentlicht in Applied sciences (01.02.2023)
    “… To realize a faster generation speed and consistency with the guidance mechanism, an improved convex optimization trajectory generation algorithm based on the flight range domain for the re-entry …”
    Volltext
    Journal Article
  8. 8

    Moon Landing Trajectory Optimization von Mustafa, Ibrahim, Shofiqul, Md

    ISSN: 2158-107X, 2156-5570
    Veröffentlicht: West Yorkshire Science and Information (SAI) Organization Limited 01.01.2016
    “… Once a trajectory is determined, guidance algorithms are created to guide the vehicle along the given trajectory …”
    Volltext
    Journal Article
  9. 9

    Lateral Vehicle Trajectory Optimization Using Constrained Linear Time-Varying MPC von Gutjahr, Benjamin, Groll, Lutz, Werling, Moritz

    ISSN: 1524-9050, 1558-0016
    Veröffentlicht: IEEE 01.06.2017
    “… In this paper, a trajectory optimization algorithm is proposed, which formulates the lateral vehicle guidance task along a reference curve as a constrained optimal control problem …”
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    Journal Article
  10. 10

    A Rapid Convex Programming Method for Air-to-Air Missile Trajectory Based on Improved Trust-Region Algorithm von Zeng Yuwen, Zhang Huijun, Liao Xueyang

    ISSN: 1673-5048
    Veröffentlicht: Editorial Office of Aero Weaponry 01.06.2025
    Veröffentlicht in Hangkong Bingqi (01.06.2025)
    “… for mid-course guidance trajectory using sequential convex programming (SCP), and designs an improved trust-region algorithm to enhance the convergence performance of the optimization …”
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    Journal Article
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    Entry trajectory optimization for hypersonic vehicle based on time-scales separation guidance with waterweeds algorithm von Xudong Liu, Lin Cheng, Qingzhen Zhang, Lingtong Jiang

    Veröffentlicht: IEEE 01.08.2016
    “… criterion based on time-scales separation guidance for oscillation optimization is put forward indicating waterweeds algorithm to get a better optimal result …”
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    Tagungsbericht
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    Constrained Reentry Trajectory Design using Whale Optimization Algorithm for Hypersonic Glide Vehicle von Dong, Chunyun, Huang, Zexian, Wu, Fangfang, Liu, Ding, Ping, Xubin

    ISSN: 1934-1768
    Veröffentlicht: Technical Committee on Control Theory, Chinese Association of Automation 24.07.2023
    Veröffentlicht in Chinese Control Conference (24.07.2023)
    “… In this paper, we attempt to handle the constrained reentry trajectory design problem using the whale optimization algorithm …”
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    Tagungsbericht
  13. 13

    Fault-Tolerant Guidance of Rocket Vertical Landing Phase Based on MPC Framework von Li, Jingqi, Long, Yaosong, Su, Mao, Liu, Lei, Wang, Bo, Cheng, Zhongtao

    ISSN: 1687-5966, 1687-5974
    Veröffentlicht: New York Hindawi 12.08.2022
    Veröffentlicht in International Journal of Aerospace Engineering (12.08.2022)
    “… In this paper, a fault-tolerant guidance method based on the MPC framework is put forward. First, we propose a piecewise guidance algorithm that combines a trajectory optimization algorithm based on convex optimization with the MPC framework …”
    Volltext
    Journal Article
  14. 14

    Convex Formulation and Efficiency Enhancement for Powered Landing Guidance With Second-Order Cone Probability Constraints von Li, Wenbo, Gong, Shengping

    ISSN: 0018-9251, 1557-9603
    Veröffentlicht: New York IEEE 01.04.2025
    “… Real-time trajectory optimization is crucial for achieving autonomous guidance in powered landing …”
    Volltext
    Journal Article
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    Midcourse Guidance Trajectory Optimization of Interceptor Missile Based on Sequential Convex Programming von Li Jiong, Zhang Jinlin, Shao Lei, Li Wanli, He Yangchao

    ISSN: 1673-5048
    Veröffentlicht: Editorial Office of Aero Weaponry 01.02.2023
    Veröffentlicht in Hangkong Bingqi (01.02.2023)
    “… Aiming at the trajectory optimization problem of interceptor midcourse guidance under strong nonlinear multi-constraint conditions, a trajectory optimization algorithm for fixed time constraints …”
    Volltext
    Journal Article
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    Analytic Calculation and Application of the Q-Law Guidance Algorithm Partial Derivatives von Shannon, Jackson L., Ellison, Donald H., Hartzell, Christine M.

    ISSN: 2195-0571, 0021-9142, 2195-0571
    Veröffentlicht: New York Springer US 17.05.2023
    Veröffentlicht in The Journal of the astronautical sciences (17.05.2023)
    “… The closed-loop Q-Law guidance algorithm has been shown to be a very capable and efficient method for producing low-thrust trajectories …”
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    Journal Article
  17. 17

    A review of optimization techniques in spacecraft flight trajectory design von Chai, Runqi, Savvaris, Al, Tsourdos, Antonios, Chai, Senchun, Xia, Yuanqing

    ISSN: 0376-0421, 1873-1724
    Veröffentlicht: Oxford Elsevier Ltd 01.08.2019
    Veröffentlicht in Progress in aerospace sciences (01.08.2019)
    “… For most atmospheric or exo-atmospheric spacecraft flight scenarios, a well-designed trajectory is usually a key for stable flight and for improved guidance and control of the vehicle …”
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    Journal Article
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    Multi-Process Integrated Planning and Guidance for Return of Reusable Aircraft Under Time Constraint von Wei, Chang-Zhu, Zhang, Ze, Li, Yuan, Li, Yongyuan

    ISSN: 2169-3536, 2169-3536
    Veröffentlicht: Piscataway IEEE 2020
    Veröffentlicht in IEEE access (2020)
    “… In this paper, a multi-process integrated (MPI) planning and guidance algorithm for deorbit phase and reentry phase is proposed to meet the mission requirement of RLV …”
    Volltext
    Journal Article
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    Control Contraction Metrics Based Robust Tracking Guidance for Hypersonic Glide Vehicle in Terminal Phase von Zhang, Haowei, Zhang, Ran, Li, Huifeng

    ISSN: 1934-1768
    Veröffentlicht: Technical Committee on Control Theory, Chinese Association of Automation 25.07.2022
    Veröffentlicht in Chinese Control Conference (25.07.2022)
    “… Then, in order to simplify the design of CCM, we choose to linearize HGV's model on the nominal trajectory and design an algorithm to solve the simplified problem using convex optimization …”
    Volltext
    Tagungsbericht
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    Real-time guidance for powered landing of reusable rockets via deep learning von Wang, Jinbo, Ma, Hongjun, Li, Huixu, Chen, Hongbo

    ISSN: 0941-0643, 1433-3058
    Veröffentlicht: London Springer London 01.03.2023
    Veröffentlicht in Neural computing & applications (01.03.2023)
    “… This paper focuses on improving the autonomy and efficiency of fuel-optimal powered landing guidance for reusable rockets considering aerodynamic forces …”
    Volltext
    Journal Article