Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, People's Republic of China.
Department of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, People's Republic of China; National Key Laboratory of Military Underwater Intelligent Robot, Harbin Engineering University, Harbin 150001, People's Republic of China.
ISA Trans. 2019 Feb;85:97-106. doi: 10.1016/j.isatra.2018.10.028. Epub 2018 Oct 27.
This paper investigates the distributed coordinated attitude tracking control problem for spacecraft formation with time-varying communication delays under the condition that the dynamic leader spacecraft is a neighbor of only a subset of follower spacecrafts. We consider two cases for the leader spacecraft: i) the attitude derivative is constant, and ii) the attitude derivative is time-varying. In the first case, a distributed estimator is proposed for each follower spacecraft by using its neighbors' information with communication delays. In the second case, to express the dynamic leader's attitude, an improved distributed observer is developed to estimate the leader's information. Based on the estimated values, adaptive coordinated attitude tracking control laws are designed to compensate for parametric uncertainties and unknown disturbances. By employing the Lyapunov-Krasovskii functional approach, the attitude tracking errors and estimation errors are proven to converge to zero asymptotically. Numerical simulations are presented to illustrate the effectiveness of theoretical results.
本文研究了在动态领航航天器仅为部分跟随航天器邻居的情况下,具有时变通信延迟的航天器编队分布式协调姿态跟踪控制问题。我们考虑了领航航天器的两种情况:i)姿态导数为常数,ii)姿态导数随时间变化。在第一种情况下,通过使用具有通信延迟的邻居信息,为每个跟随航天器提出了一种分布式估计器。在第二种情况下,为了表示动态领航器的姿态,开发了一种改进的分布式观测器来估计领航器的信息。基于估计值,设计了自适应协调姿态跟踪控制律来补偿参数不确定性和未知干扰。通过使用 Lyapunov-Krasovskii 泛函方法,证明了姿态跟踪误差和估计误差渐近收敛到零。数值模拟结果表明了理论结果的有效性。