宇航学报
宇航學報
우항학보
JOURNAL OF ASTRONAUTICS
2010年
1期
143-147
,共5页
交会对接%滑模控制%绕飞%分时控制
交會對接%滑模控製%繞飛%分時控製
교회대접%활모공제%요비%분시공제
Rendezvous & docking%Slide-mode-control%Flying-around%Time sharing control
基于多模态滑模控制的理念,研究了交会对接绕飞段的控制问题.介绍了多模态滑模切换函数的设计方法,并给出滑模面的存在条件和系统稳定性证明.采用分时控制方法弱化系统变量之间的耦合,简化了控制系统的设计.对该控制系统进行了数值仿真,结果表明:系统可以经由预想的绕飞轨线,由初态绕飞至终态,而且对初始状态具有很好的适应性.
基于多模態滑模控製的理唸,研究瞭交會對接繞飛段的控製問題.介紹瞭多模態滑模切換函數的設計方法,併給齣滑模麵的存在條件和繫統穩定性證明.採用分時控製方法弱化繫統變量之間的耦閤,簡化瞭控製繫統的設計.對該控製繫統進行瞭數值倣真,結果錶明:繫統可以經由預想的繞飛軌線,由初態繞飛至終態,而且對初始狀態具有很好的適應性.
기우다모태활모공제적이념,연구료교회대접요비단적공제문제.개소료다모태활모절환함수적설계방법,병급출활모면적존재조건화계통은정성증명.채용분시공제방법약화계통변량지간적우합,간화료공제계통적설계.대해공제계통진행료수치방진,결과표명:계통가이경유예상적요비궤선,유초태요비지종태,이차대초시상태구유흔호적괄응성.
The control for flying-around of rendezvous and docking was researched based on the concept of Multi-Sliding-Mode (MSM) control. The design for switching function of MSM was introduced, the existence condition for sliding mode was given and the stability of the control system was proved. For decreasing the couplings between the system variables, time sharing control was used, the design for control system was simplified. The control system was simulated and the results show that the system could be transferred from initial state to final state along the expected flying-around trajectory and has good adaptability for different initial states.