摘要
针对停靠阶段追踪飞行器轨道与姿态动力学和控制耦合问题 ,在两种控制律作用下进行了研究 ,给出了轨道动力学和姿态动力学模型以及四元数表示的姿态运动学模型。所给出的一个仿真算例表明 。
The dynamics and control couple of orbit and attitude during final approach phase is an important problem which is discussed under two control laws in this paper. Both the dynamics equations of orbit and attitude and the attitude kinetics model based on quaternion are given. A numerical example is also given and the simulation results show the effectiveness of the proposed control laws.
出处
《飞行力学》
CSCD
2002年第1期33-37,共5页
Flight Dynamics
