Large Angular Autonomous Attitude Maneuver of Deep spacecraft using Pseudospectral Method
An autonomous large angular slew of deep spacecraft is studied, which is a key factor in the development of future spacecraft autonomous platform. The objective is to minimize some performance index and rotate the spacecraft to a desired attitude while subject to dynamic and geometric constraints. The investigated literature did not handle this problem very well either in performance or constraints consideration. In this paper, we propose a new approach based on pseudospectral method for autonomous attitude control, not only satisfies the nonconvex constraints but also optimizes performance. We approach this by two stages: (1) get the feasible path using RRT in Rodrigues space and (2) transform the optimal control problem to a nonlinear planning problem (NLP) utilizing Pseudospectral method. Finally, attitude path is obtained by solving the NLP with an initial value from (1). Simulation example is presented and discussed.
Cheng Xiaojun Cui Hutao Cui Pingyuan Xu Rui
Deep Space Exploration Research Center,Harbin Institute of Technology,Harbin,150001,China. School of Aerospace Engineering,Beijing Institute of Technology,Beijing,100081,China.
国际会议
哈尔滨
英文
1498-1502
2010-01-08（万方平台首次上网日期，不代表论文的发表时间）