Nonlinear Algorithm for Tracking Interplanetary Low-Thrust Trajectories

被引：5
|
作者：
Huang, Rosemary C. [1 ]
Hwang, Inseok [1 ]
Corless, Martin J. [1 ]
机构：
[1] Purdue Univ, Sch Aeronaut & Astronaut, W Lafayette, IN 47907 USA
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2012年 / 35卷 / 02期
关键词：
GUIDANCE;
D O I：
10.2514/1.53001
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A nonlinear trajectory tracking algorithm introduced here has been successfully applied to the low-thrust transfer problem. The algorithm is an application of the NMPC (nonlinear model predictive control) method where the solution to the optimal control subproblem is found through the DT(differential transformation) method. It is able to track a nominal trajectory in spite of a disturbance from unmodeled solar radiation pressure. Additionally, the algorithm has been shown to be more robust to state measurement delays than a LQR (linear quadratic regulator).
引用
收藏
页码：696 / 700
页数：5
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