[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

弹箭与制导学报 >

2010 , Vol. 30 >Issue 1: 51 - 53,57

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.01.007

导弹与制导技术

可重复使用运载器的RCS 姿态控制技术研究

  • 贺成龙 ,
  • 陈欣 ,
  • 吴了泥
展开
  • 南京航空航天大学自动化学院,南京 210016

贺成龙(1980-),男,湖南人,博士研究生,研究方向:无人机飞行控制,可重复使用运载器制导与控制。

收稿日期: 2009-04-29

  网络出版日期: 2025-05-19

基金资助

国家863高新技术项目资助

收起

Research on Attitude Control of Reaction Control System for Reusable Launch Vehicle

  • HE Chenglong ,
  • CHEN Xin ,
  • WU Liaoni
Expand
  • College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Received date: 2009-04-29

  Online published: 2025-05-19

Fold

摘要

反作用控制系统作为可重复使用运载器高空的姿态控制手段,其力矩特性不同于常规的气动操纵面,因此设计适合高空姿态控制特点与要求的控制系统是非常必要的。文中采用了一种带死区的乒乓控制方式,设计了俯仰、滚转和偏航的反馈控制律,采用描述函数法在频率上分析了控制系统的稳定性。仿真结果表明,设计的控制系统能较好的满足高空姿态控制要求,最后对姿态控制效果和反作用控制系统喷量之间的关系进行了分析。

关键词： 可重复使用运载器; 反作用控制系统; 姿态控制; 乒乓控制; 描述函数法

本文引用格式

贺成龙 , 陈欣 , 吴了泥 . 可重复使用运载器的RCS 姿态控制技术研究[J]. 弹箭与制导学报, 2010 , 30(1) : 51 -53,57 . DOI: 10.15892/j.cnki.djzdxb.2010.01.007

Abstract

Reaction control system (RCS) is used for reusable launch vehicle (RLV)' attitude control, which is different from the atmospheric steers control, so a well designed control system to fit the attitude control in high altitude is required. In this Paper, a ping pong control structure with dead zone was proposed for attitude control, angular motion was simplified in order to convenient for control law designing, the feedback control laws for pitching, rolling and yawing were designed, and the stability of the whole control system was analyzed using describing function method. Simulation shows that the control system is satisfied, finally, Comparison between the attitude control effect and jet flux was analyzed.

Key words： RLV; RCS; attitude control; ping pong control; describing function method

[an error occurred while processing this directive]

参考文献

[1]
宁国栋, 张曙光. 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.
[2]
呼卫军, 周军. 可重复使用运载器 RCS 修正脉冲调宽算法研究[J]. 弹箭与制导学报, 2006, 26 (4): 313- 316.
[3]
T Ting, N Flanagan. Space shuttle transition controller OMS-TVC and RCS jet thruster stability analysis[R]. AIAA-91-2220.
[4]
V E Haloulakos. Thrust and impulse requirements for jetattitude control systems[R]. AIAA 63-237.
[5]
Joe D Gamble, Kenneth M Spratlin, Lisa M. Skalecki. Lateral directional requirements for a low L D aero-ma- neuvering orbital transfer vehicle[R]. AIAA 84-2123.
[6]
R Taylor. Adaptive attitude control for long-life space vehicles[R]. AIAA 69-945.
[7]
Bernelli-Zazzera F, Paolo Mantegazza P. Pulse width e- quivalent to pulse-amplitude discrete control of linear system[J]. Journal of Guidance, Control and Dynamics, 1992, 15 (2): 461- 467.
[8]
方振平, 陈万春, 张曙光. 航空飞行器飞行动力学[M]. 北京: 北京航天航空大学出版社, 2005.
[9]
Gu Yingsong, Yang Zhichun. Aeroelastic analysis of an airfoil with a hysteresis non-linearity[C]// 47th IAA/ ASM/ASCE/AHS/ASC Structures, Structural Dynam- ics, and Materials Con, 2006.
[10]
T Ueda, E H Dowell. Flutter analysis using nonlinear aerodynamic forces[R]. ALAA 82-0728.
Options
文章导航

/

〈 〉

[an error occurred while processing this directive]