| 跨大气层飞行器再入段RCS控制特性 |
| |
| 引用本文： | 宁国栋,张曙光,方振平.跨大气层飞行器再入段RCS控制特性[J].飞行力学,2005,23(3):16-20. |
| |
| 作者姓名： | 宁国栋 张曙光 方振平 |
| |
| 作者单位： | 北京航空航天大学,航空科学与工程学院,北京,100083 |
| |
| 摘 要： | 以航天飞机为例．论述了跨火气层飞行器反推力控制系统（Reaction Control System，RCS）的工作原理，并给出了RCS推进器的控制模型。同时分析了RCS在回路中的各种工作模式和多推进器的系统冗余及其组合方式。最后在对RCS系统操作的基础上，研究了航天飞机在再人段飞行时的RCS控制问题。
|
| 关 键 词： | 反推力控制系统 飞行控制 系统冗余 再入段飞行 |
| 文章编号： | 1002-0853(2005)03-0016-05 |
| 收稿时间： | 2004-07-12 |
| 修稿时间： | 2005-04-22 |
Research on the Reaction Control System for Spacecraft Re-Entry Flight |
| |
| NING Guo-dong,ZHANG Shu-guang,FANG Zhen-ping.Research on the Reaction Control System for Spacecraft Re-Entry Flight[J].Flight Dynamics,2005,23(3):16-20. |
| |
| Authors: | NING Guo-dong ZHANG Shu-guang FANG Zhen-ping |
| |
| Abstract: | The operating principle of the Reaction Control System (RCS) for a spacecraft was discussed, and the control model of RCS jets was presented. According to the example of American Space Shuttle, the modes of RCS in closed loop, the system redundancy and compound mode of multi-jets were analyzed. And based on the system operation of RCS, some problems of RCS control and availability of actuators for spacecraft re-entry flight were performed. |
| |
| Keywords: | reaction control system flight control system redundancy re-entry flight |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
