| 相对运动有限推力轨道控制 |
| |
| 引用本文： | 荆武兴,杨涤.相对运动有限推力轨道控制[J].宇航学报,1993,14(2):35-41. |
| |
| 作者姓名： | 荆武兴 杨涤 |
| |
| 作者单位： | 哈尔滨工业大学，哈尔滨工业大学，哈尔滨工业大学 哈尔滨 150006，哈尔滨 150006，哈尔滨 150006 |
| |
| 摘 要： |
|
| 关 键 词： | 反馈控制逻辑 轨道 控制 有限推力 |
FINITE THRUST ORBITAL CONTROL IN RELATIVE MOTION |
| |
| Jing Wuxing Yang Di Wu Yaohua.FINITE THRUST ORBITAL CONTROL IN RELATIVE MOTION[J].Journal of Astronautics,1993,14(2):35-41. |
| |
| Authors: | Jing Wuxing Yang Di Wu Yaohua |
| |
| Abstract: | Orbital control of chasing spacecraft during relative motion is studied. Thrust value of actuator is supposed to be constant. State feedback on-off contrrol logic is presented by using maximum principle. Simulation example is provided to illustrate feasibility of the control logic. |
| |
| Keywords: | Feedback control logic Orbital control Finite thrust Optimal control |
| 本文献已被 CNKI 维普 等数据库收录！ |
