小天体柔性附着强耦合系统协同博弈控制

Translated title of the contribution: Game-based Control of Strongly Coupled System for Flexible Landing on Small Celestial Body

Chengyu Zhang, Zixuan Liang*, Shengying Zhu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

To deal with the strong nonlinear attitude-orbit coupling control problem of a flexible lander,a multi-thruster game-based control method is proposed. This method achieves integrated control of attitude and trajectory motion by coordinating the control inputs of multiple thrusters. Firstly,the control strategies interaction of multi-thrusters is realized based on the differential game framework. This framework introduces dynamic prediction information of the system in cooperative control law design,thereby avoiding conflicts and redundancies in multi-thruster control. Therefore,both the overall attitude-orbit performance of the flexible lander and the control energy of each thruster are improved. Secondly,based on sequential approximation and quasi-linearization techniques,a successive approximation-based parameter search algorithm is designed. This algorithm yields closed-form game-based feedback control laws in the presence of strong coupling nonlinearity. As a result,control commands can be autonomously computed onboard. Finally,using a landing scenario on asteroid 433 Eros,the effectiveness of game-based control is validated through numerical simulation.

Translated title of the contributionGame-based Control of Strongly Coupled System for Flexible Landing on Small Celestial Body
Original languageChinese (Traditional)
Pages (from-to)1775-1788
Number of pages14
JournalYuhang Xuebao/Journal of Astronautics
Volume45
Issue number11
DOIs
Publication statusPublished - Nov 2024

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