载人航天
載人航天
재인항천
MANNED SPACEFLIGHT
2015年
5期
456-461
,共6页
遥操作%交会对接%相平面控制%时延
遙操作%交會對接%相平麵控製%時延
요조작%교회대접%상평면공제%시연
teleoperation%rendezvous and docking%phase plane control%time delay
以时延条件下的地球轨道遥操作交会对接为背景,针对遥操作交会对接中时延引起的控制系统不稳定问题,开展了交会平移靠拢段的控制策略研究,在基于C-W方程的预测显示模型基础上,设计了平移靠拢段纵向速度曲线控制及横向位置-速度的相平面控制算法. 仿真表明,该方法能有效克服大时延影响,具有较好控制效果,且算法简单可靠,易于工程实现.
以時延條件下的地毬軌道遙操作交會對接為揹景,針對遙操作交會對接中時延引起的控製繫統不穩定問題,開展瞭交會平移靠攏段的控製策略研究,在基于C-W方程的預測顯示模型基礎上,設計瞭平移靠攏段縱嚮速度麯線控製及橫嚮位置-速度的相平麵控製算法. 倣真錶明,該方法能有效剋服大時延影響,具有較好控製效果,且算法簡單可靠,易于工程實現.
이시연조건하적지구궤도요조작교회대접위배경,침대요조작교회대접중시연인기적공제계통불은정문제,개전료교회평이고롱단적공제책략연구,재기우C-W방정적예측현시모형기출상,설계료평이고롱단종향속도곡선공제급횡향위치-속도적상평면공제산법. 방진표명,해방법능유효극복대시연영향,구유교호공제효과,차산법간단가고,역우공정실현.
Based on the problem of ground-based teleoperation rendezvous and docking in earth orbit with time delay,this paperfocused on the delay-induced instability of control system on teleoperation rendezvous and docking. The strategy of orbit control in the final approach phase was studied. A predictive model was established based on the Clohessy-Wiltshire equations. The longitudinal veloci-ty control algorithm and transverse position-velocity control algorithms were proposed based on the previous predictive model. Simulation results show that the control method is effective in alleviating the influence of time delay and the success probability is improved. The algorithm is proved to be simple and reliable, and can be easily implemented in engineering.