Finite Horizon Optimal Nonlinear Spacecraft Attitude Control

被引：0
作者：
Ahmed Khamis
Dawid Zydek
机构：
[1] Military Technical College,
[2] University of Nevada,undefined
来源：
The Journal of the Astronautical Sciences | 2020年 / 67卷
关键词：
SDRE; Nonlinear control; Spacecraft attitude control;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
This research is devoted to present spacecraft attitude control via a finite-horizon nonlinear optimal control technique. The spacecraft kinematics are represented using the modified Rodrigues parameters, which possess singularities for eigenaxis rotations greater than 180 degree. The proposed technique is based on State Dependent Riccati Equation (SDRE). In this technique, the differential Riccati equation is converted to a linear Lyapunov differential equation. This technique can be applied for finite-horizon nonlinear regulation and tracking problems. The proposed technique is effective for a wide range of operating points. Simulation results are given to illustrate the effectiveness of the finite horizon technique.
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页码：1002 / 1020
页数：18
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