ACTA AERONAUTICAET ASTRONAUTICA SINICA >
A high⁃order fully actuated predictive control approach of spacecraft flying⁃around under time⁃variant communication constraints
Received date: 2023-02-28
Revised date: 2023-04-11
Accepted date: 2023-05-11
Online published: 2023-05-17
Supported by
National Natural Science Foundation of China(62173255)
A High-Order Fully Actuated （HOFA） predictive control approach is proposed for the problem of spacecraft flying-around under time-variant communication constraints in a sight coordinate system， including both time-variant communication delays and time-variant packets dropouts in the communication channels between the servicing spacecraft and the tracking and data relay satellite system. In the sight coordinate system， a nonlinear HOFA system model is introduced to describe the relative dynamics of spacecraft flying-around， such that the proposed flying-around task can be considered as a tracking control problem of nonlinear HOFA system. In this approach， the nonlinearities can be eliminated to construct a linear HOFA system because of full actuation characteristic， and then a Linear Incremental HOFA （LIHOFA） prediction model is constructed by applying a Diophantine Equation to replace a reduced-order prediction model， such that multi-step ahead predictions are developed to achieve the optimization of tracking control performance and the compensation of time-variant communication constraints， which guarantees the realization of this flying-around mission. A necessary and sufficient condition is given to analyze the stability and tracking performance of closed-loop system. Further， two simulated examples of spacecraft flying-around in circular and elliptical orbits are provided to verify the feasibility of HOFA predictive control approach.
Dawei ZHANG , Guoping LIU . A high⁃order fully actuated predictive control approach of spacecraft flying⁃around under time⁃variant communication constraints[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2024 , 45(1) : 628633 -628633 . DOI: 10.7527/S1000-6893.2023.28633
| 1 | 胡庆雷， 邵小东， 杨昊旸， 等. 航天器多约束姿态规划与控制：进展与展望［J］. 航空学报， 2022， 43（10）： 527351. |
| HU Q L， SHAO X D， YANG H Y， et al. Spacecraft attitude planning and control under multiple constraints： Review and prospects［J］. Acta Aeronautica et Astronautica Sinica， 2022， 43（10）： 527351 （in Chinese）. | |
| 2 | 李敏，袁利，魏春岭. 基于混合状态机的航天器自主绕飞多模态控制［J］. 航空学报， 2023， 44（18）： 328296. |
| LI M， YUAN L， WEI C L. Spacecraft autonomous fly-around multi-mode control based-on hybrid state machine［J］. Acta Aeronautica et Astronautica Sinica， 2023， 44（18）： 328296. | |
| 3 | ZHANG D W， LIU G P. Output feedback predictive control for discrete quasilinear systems with application to spacecraft flying-around［J］. Asian Journal of Control， 2022， 24（4）： 1846-1861. |
| 4 | ZHANG D W， LIU G P. Coordinated control of quasilinear multiagent systems via output feedback predictive control［J］. ISA Transactions， 2022， 128： 58-70. |
| 5 | HUANG Y， JIA Y M. Adaptive finite-time 6-DOF tracking control for spacecraft fly around with input saturation and state constraints［J］. IEEE Transactions on Aerospace and Electronic Systems， 2019， 55（6）： 3259-3272. |
| 6 | HUANG Y， JIA Y M. Adaptive fixed-time six-DOF tracking control for noncooperative spacecraft fly-around mission［J］. IEEE Transactions on Control Systems Technology， 2019， 27（4）： 1796-1804. |
| 7 | SU Y Z， YANG Y J， YANG X R， et al. Attitude tracking control for observation spacecraft flying around the target spacecraft［J］. IET Control Theory & Applications， 2021， 15（14）： 1868-1881. |
| 8 | WANG Y， JI H B. Input-to-state stability-based adaptive control for spacecraft fly-around with input saturation［J］. IET Control Theory & Applications， 2020， 14（10）： 1365-1374. |
| 9 | ZHANG R， HAN C， RAO Y R， et al. Spacecraft fast fly-around formations design using the bi-teardrop configuration［J］. Journal of Guidance， Control， and Dynamics， 2018， 41（7）： 1542-1555. |
| 10 | HUANG Y， JIA Y M. Robust adaptive fixed-time tracking control of 6-DOF spacecraft fly-around mission for noncooperative target［J］. International Journal of Robust and Nonlinear Control， 2018， 28（6）： 2598-2618. |
| 11 | LIU L， LIU J G， WU Y M. Event-triggered coordinated control for multiple solar sail formation flying around planetary displaced orbits［J］. Acta Astronautica， 2021， 184： 286-298. |
| 12 | WANG W， BAOYIN H X， MENGALI G， et al. Solar sail cooperative formation flying around L2-type artificial equilibrium points［J］. Acta Astronautica， 2020， 169： 224-239. |
| 13 | 刘国平. 具有时变通信受限非线性信息物理系统的网络化预测控制［J］. 控制理论与应用， 2022， 39（1）： 145-153. |
| LIU G P. Networked predictive control of nonlinear cyber physical systems with time-varying communication constraints［J］. Control Theory & Applications， 2022， 39（1）： 145-153 （in Chinese）. | |
| 14 | GU Z， YAN S， AHN C K， et al. Event-triggered dissipative tracking control of networked control systems with distributed communication delay［J］. IEEE Systems Journal， 2022， 16（2）： 3320-3330. |
| 15 | MASTANI E， RAHMANI M. Dynamic output feedback control for networked systems subject to communication delays， packet dropouts， and quantization［J］. Journal of the Franklin Institute， 2021， 358（8）： 4303-4325. |
| 16 | ZHAO Z Y， YI X J， MA L F， et al. Quantized recursive filtering for networked systems with stochastic transmission delays［J］. ISA Transactions， 2022， 127： 99-107. |
| 17 | DUAN G R. High-order fully actuated system approaches： Part I. Models and basic procedure［J］. International Journal of Systems Science， 2021， 52（2）： 422-435. |
| 18 | ZHANG D W， LIU G P， CAO L. Coordinated control of high-order fully actuated multiagent systems and its application： A predictive control strategy［J］. IEEE/ASME Transactions on Mechatronics， 2022， 27（6）： 4362-4372. |
| 19 | ZHANG D W， LIU G P， CAO L. Constrained cooperative control for high-order fully actuated multiagent systems with application to air-bearing spacecraft simulators［J］. IEEE/ASME Transactions on Mechatronics， 2023， 28（3）： 1570-1581. |
| 20 | MENG R， HUA C C， LI K， et al. Adaptive event-triggered control for uncertain high-order fully actuated system［J］. IEEE Transactions on Circuits and Systems II： Express Briefs， 2022， 69（11）： 4438-4442. |
| 21 | DUAN G Q， LIU G P. Attitude and orbit optimal control of combined spacecraft via a fully-actuated system approach［J］. Journal of Systems Science and Complexity， 2022， 35（2）： 623-640. |
| 22 | 刘暾， 赵钧. 空间飞行器动力学［M］. 哈尔滨： 哈尔滨工业大学出版社， 2003： 83-86. |
| LIU T， ZHAO J. Dynamics of Spacecraft［M］. Harbin： Harbin Institute of Technology Press， 2003： 83-86 （in Chinese）. | |
| 23 | DUAN G R. High-order fully actuated system approaches： Part X. Basics of discrete-time systems［J］. International Journal of Systems Science， 2022， 53（4）： 810-832. |
| 24 | ZHANG D W， LIU G P. Predictive control for networked high-order fully actuated systems subject to communication delays and external disturbances［J］. ISA Transactions， 2023， 139： 425-435. |
| 25 | ZHANG D W， LIU G P， CAO L. Predictive control of discrete-time high-order fully actuated systems with application to air-bearing spacecraft simulator［J］. Journal of the Franklin Institute， 2023， 360（8）： 5910-5927. |
| 26 | ZHANG D W， LIU G P， CAO L. Proportional integral predictive control of high-order fully actuated networked multiagent systems with communication delays［J］. IEEE Transactions on Systems， Man， and Cybernetics： Systems， 2023， 53（2）： 801-812. |
| 27 | AMATO F， COSENTINO C， DE TOMMASI G， et al. Input?output finite-time stabilization of linear time-varying discrete-time systems［J］. IEEE Transactions on Automatic Control， 2022， 67（9）： 4438-4450. |
| 28 | BABIARZ A， CZORNIK A， SIEGMUND S. On stabilization of discrete time-varying systems［J］. SIAM Journal on Control and Optimization， 2021， 59（1）： 242-266. |
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