Trajectory Control of Midcourse Guidance for Air-to-Air Missile Based on Feedback Linearization and Sliding Mode Control

To guarantee the accuracy and energy efficiency of long-distance midcourse guidance for air-to-air missile, a robust trajectory control method based on feedback linearization and sliding mode control is proposed. In guidance loop, the framework of offline trajectory optimization and online tracking...

Full description

Saved in:
Bibliographic Details
Published in:Proceedings of ... IEEE International Conference on Unmanned Systems (Online) pp. 1887 - 1892
Main Authors: Zhang, Chencheng, Tong, Zhiqiang, Liu, Hongquan, Pang, Weijian
Format: Conference Proceeding
Language:English
Published: IEEE 18.10.2024
Subjects:
air-to-air missile
Atmospheric modeling
Feedback linearization
midcourse guidance
Missiles
Nonlinear dynamical systems
Perturbation methods
Robustness
Sliding mode control
Tracking loops
trajectory control
Trajectory optimization
Trajectory planning
ISSN:2771-7372
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Abstract To guarantee the accuracy and energy efficiency of long-distance midcourse guidance for air-to-air missile, a robust trajectory control method based on feedback linearization and sliding mode control is proposed. In guidance loop, the framework of offline trajectory optimization and online tracking control is introduced and the nominal optimal trajectory is obtained by Gauss pseudo-spectral method. In control loop, based on the fact that the velocity profile of tactical missile is untracked, the model is reduced to only depending on flight path angle and height. Furthermore, the reduced complex nonlinear dynamics are accurately linearized by feedback linearization. To overcome the multiple disturbances and parameter perturbation, sliding mode control is introduced to improve the robustness. The global asymptotic stability of the resulting control law is proved. The efficiency and robustness are verified by multiple simulations under the conditions of initial errors, random wind disturbance model, and parameter perturbation.
AbstractList To guarantee the accuracy and energy efficiency of long-distance midcourse guidance for air-to-air missile, a robust trajectory control method based on feedback linearization and sliding mode control is proposed. In guidance loop, the framework of offline trajectory optimization and online tracking control is introduced and the nominal optimal trajectory is obtained by Gauss pseudo-spectral method. In control loop, based on the fact that the velocity profile of tactical missile is untracked, the model is reduced to only depending on flight path angle and height. Furthermore, the reduced complex nonlinear dynamics are accurately linearized by feedback linearization. To overcome the multiple disturbances and parameter perturbation, sliding mode control is introduced to improve the robustness. The global asymptotic stability of the resulting control law is proved. The efficiency and robustness are verified by multiple simulations under the conditions of initial errors, random wind disturbance model, and parameter perturbation.
Author Zhang, Chencheng
Tong, Zhiqiang
Pang, Weijian
Liu, Hongquan
Author_xml – sequence: 1
  givenname: Chencheng
  surname: Zhang
  fullname: Zhang, Chencheng
  email: zhangchencheng@nuaa.edu.cn
  organization: College of Automation Engineering, Nanjing University of Aeronautics and Astronautics,Nanjing,China
– sequence: 2
  givenname: Zhiqiang
  surname: Tong
  fullname: Tong, Zhiqiang
  email: 407386992@qq.com
  organization: Air force Research Institute,Beijing,China
– sequence: 3
  givenname: Hongquan
  surname: Liu
  fullname: Liu, Hongquan
  email: liuhq03@126.com
  organization: Air force Research Institute,Beijing,China
– sequence: 4
  givenname: Weijian
  surname: Pang
  fullname: Pang, Weijian
  email: pangweijian2013@163.com
  organization: Air force Research Institute,Beijing,China
BookMark eNo1UM1KAzEYjKKg1r6BYF5ga362m-RYF1sLLR5az-Xb5Iukrolkt2B9ele0p4GZYYaZG3IRU0RC7jmbcM7Mw7J-3VRcyWoimCgnnOmScSnOyNgoo-WUSV1yPT0n10IpXiipxBUZd92eMSYFGzR1Tb62GfZo-5SPtE6xz6mlydN1cDYdcod0cQgOokXqU6azkIs-FQMMjq4LLdJH6NDRFOkc0TVg3-kqRIQcvqEPAw3R0U0bXIhvdJ0cnlpuyaWHtsPxP47Idv60rZ-L1ctiWc9WRTC8L7zTHiwXYBSz2qPkUAIbWHSKYTVMnirRWEBsZFn9Gq0ppdeWmaqqoJEjcvcXGxBx95nDB-Tj7vSV_AF7VmG6
ContentType Conference Proceeding
DBID 6IE
6IL
CBEJK
RIE
RIL
DOI 10.1109/ICUS61736.2024.10840132
DatabaseName IEEE Electronic Library (IEL) Conference Proceedings
IEEE Xplore POP ALL
IEEE Xplore All Conference Proceedings
IEEE/IET Electronic Library
IEEE Proceedings Order Plans (POP All) 1998-Present
DatabaseTitleList
Database_xml – sequence: 1
  dbid: RIE
  name: IEEE Electronic Library (IEL)
  url: https://ieeexplore.ieee.org/
  sourceTypes: Publisher
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
EISBN 9798350384185
9798350384178
EISSN 2771-7372
EndPage 1892
ExternalDocumentID 10840132
Genre orig-research
GrantInformation_xml – fundername: National Natural Science Foundation of China
  grantid: 62233009,62303218
  funderid: 10.13039/501100001809
GroupedDBID 6IE
6IF
6IL
6IN
AAWTH
ABLEC
ADZIZ
ALMA_UNASSIGNED_HOLDINGS
BEFXN
BFFAM
BGNUA
BKEBE
BPEOZ
CBEJK
CHZPO
IEGSK
OCL
RIE
RIL
ID FETCH-LOGICAL-i91t-fd8fac12a970c8fe31a4a0fd8ed70e6084572bcaeeb346c12ac943f8c09666ab3
IEDL.DBID RIE
IngestDate Wed Jan 29 10:31:17 EST 2025
IsPeerReviewed false
IsScholarly true
Language English
LinkModel DirectLink
MergedId FETCHMERGED-LOGICAL-i91t-fd8fac12a970c8fe31a4a0fd8ed70e6084572bcaeeb346c12ac943f8c09666ab3
PageCount 6
ParticipantIDs ieee_primary_10840132
PublicationCentury 2000
PublicationDate 2024-Oct.-18
PublicationDateYYYYMMDD 2024-10-18
PublicationDate_xml – month: 10
  year: 2024
  text: 2024-Oct.-18
  day: 18
PublicationDecade 2020
PublicationTitle Proceedings of ... IEEE International Conference on Unmanned Systems (Online)
PublicationTitleAbbrev ICUS
PublicationYear 2024
Publisher IEEE
Publisher_xml – name: IEEE
SSID ssj0003204187
Score 2.2713108
Snippet To guarantee the accuracy and energy efficiency of long-distance midcourse guidance for air-to-air missile, a robust trajectory control method based on...
SourceID ieee
SourceType Publisher
StartPage 1887
SubjectTerms air-to-air missile
Atmospheric modeling
Feedback linearization
midcourse guidance
Missiles
Nonlinear dynamical systems
Perturbation methods
Robustness
Sliding mode control
Tracking loops
trajectory control
Trajectory optimization
Trajectory planning
Title Trajectory Control of Midcourse Guidance for Air-to-Air Missile Based on Feedback Linearization and Sliding Mode Control
URI https://ieeexplore.ieee.org/document/10840132
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://cvtisr.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwlV07T8MwELagYoCFVxFveWB1iRMT2yNUFJCgqtQidasc-ywFUIJKiuDfc07TAgMDUyLLlh-fzp_vfOcj5EwK3AC4cSxzQjCBCgYzWiRMKOudVWkWQY30vez31XisB02weh0LAwC18xl0wm99l-9KOwumMpRwFdQB3HFXpZTzYK2lQSWJI8GVbHy4eKTP77qPQyToJHgixKKzaP0rj0pNI73Nfw5gi7S_A_LoYEk122QFih2y8eMtwV3ygazzVJvgP2l37n9OS08fcmfL4KhBb2a5CxBTPKbSy3zKqpLhB2ugWLwAvUI-c7QsaA97yYx9pqinohw0gZrUFI4OX_IwABoyqC16aZNR73rUvWVNWgWWa14x75Q3lsdGy8gqDwk3wkRYCk4iMDjDCxln1gCq2SINFS2C55VFZSdNTZbskVZRFrBPKB4mMuscBy20AMVNHHkAraVLImNjeUDaYQ0nr_OHMyaL5Tv8o_yIrAekAjVwdUxa1XQGJ2TNvlf52_S0hvsLYEytKQ
linkProvider IEEE
linkToHtml http://cvtisr.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwlV07T8MwELZQQQIWXkW88cDqEiduYo9QUVrRVpVapG6VY1-kQJWgkiL495zTlMfAwJTIsuXHp_PnO9_5CLmKBG4AXFsWWyGYQAWDaSUCJqRJrJFh7EGJdC8aDORkooZVsHoZCwMApfMZNNxveZdvc7NwpjKUcOnUAdxx15tC-HwZrvVlUgl8T3AZVV5c3FPX3dbjCCk6cL4Ivmis2v_KpFISSXvnn0PYJfXvkDw6_CKbPbIG2T7Z_vGa4AF5R955Ko3wH7S19ECneUL7qTW5c9Wg94vUOpApHlTpTTpnRc7wgzVQMGZAb5HRLM0z2sZeYm2eKWqqKAlVqCbVmaWjWeoGQF0OtVUvdTJu341bHVYlVmCp4gVLrEy04b5WkWdkAgHXQntYCjZCaHCGzciPjQZUtEXoKhqEL5EG1Z0w1HFwSGpZnsERoXiciI21HJRQAiTXvpcAKBXZwNPGj45J3a3h9GX5dMZ0tXwnf5Rfks3OuN-b9rqDh1Oy5VBzRMHlGakV8wWckw3zVqSv84sS-k-NMrBw
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%3Abook&rft.genre=proceeding&rft.title=Proceedings+of+...+IEEE+International+Conference+on+Unmanned+Systems+%28Online%29&rft.atitle=Trajectory+Control+of+Midcourse+Guidance+for+Air-to-Air+Missile+Based+on+Feedback+Linearization+and+Sliding+Mode+Control&rft.au=Zhang%2C+Chencheng&rft.au=Tong%2C+Zhiqiang&rft.au=Liu%2C+Hongquan&rft.au=Pang%2C+Weijian&rft.date=2024-10-18&rft.pub=IEEE&rft.eissn=2771-7372&rft.spage=1887&rft.epage=1892&rft_id=info:doi/10.1109%2FICUS61736.2024.10840132&rft.externalDocID=10840132