Reaction Control System Design for Unsymmetric Flexible Spacecraft with Consideration of Torque Arm Perturbation

Shigemune Taniwaki; Shinichiro Ichikawa; Yoshiaki Ohkami

首页> 外文期刊>日本航空宇宙学会論文集 >Reaction Control System Design for Unsymmetric Flexible Spacecraft with Consideration of Torque Arm Perturbation

【24h】

Reaction Control System Design for Unsymmetric Flexible Spacecraft with Consideration of Torque Arm Perturbation

机译：考虑转矩臂摄动的非对称挠性航天器反作用控制系统设计

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

Unsymmetric flexible spacecrafts have particular dynamic characteristics; when the attitude control actuactor such as RCS thruster is used, the imbalance between negative torque and positive torque is caused. And even worse, an inertia matrix and a coupling matrix are changed depending on the displacement of the rotation paddle and the mobile sensor. In this paper, an attitude control system with consideration of these characteristics is proposed.

机译：不对称的挠性航天器具有特殊的动力学特性。当使用RCS推进器等姿态控制执行器时，会引起负扭矩和正扭矩之间的不平衡。甚至更糟的是，惯性矩阵和耦合矩阵根据旋转桨和移动传感器的位移而改变。本文提出了一种考虑到这些特性的姿态控制系统。

著录项

来源
《日本航空宇宙学会論文集》 |2000年第560期|p.308-313|共6页
作者
Shigemune Taniwaki; Shinichiro Ichikawa; Yoshiaki Ohkami;
展开▼
作者单位

展开▼
收录信息
原文格式 PDF
正文语种 jpn
中图分类航空;
关键词
spacecraft; attitude control; flexible structure;

机译：航天器态度控制灵活的结构;

相似文献

外文文献
中文文献
专利

1. Reaction Control System Design for Unsymmetric Flexible Spacecraft with Consideration of Torque Arm Perturbation [J] . Shigemune Taniwaki, Shinichiro Ichikawa, Yoshiaki Ohkami 日本航空宇宙学会論文集 . 2000,第560期

机译：考虑转矩臂摄动的非对称挠性航天器反作用控制系统设计
2. Force sensorless control in a flexible link arm based on estimated reaction torque [J] . Masaaki Shibata, Kenichi Isomura, Toshiyuki Murakami 精密工学会誌 . 1997,第2期

机译：基于估计的反作用扭矩的柔性连杆臂中的无传感器控制
3. An autonomous charge control system at geosynchronous altitude: flight results for spacecraft design consideration [J] . Mullen E.G., Frederickson A.R. IEEE Transactions on Nuclear Science . 1997,第6期

机译：地球同步高度的自动充电控制系统：考虑航天器设计的飞行结果
4. Thruster Modulation for Unsymmetric Flexible Spacecraft with Consideration of Torque Arm Perturbation [C] . Shigemune Taniwaki, Shinichiro Ichikawa, Yoshiaki Ohkami International conference on dynamics and control of systems and structures in space . 2002

机译：考虑到扭矩手臂扰动的非对称柔性宇宙飞船推进器调制
5. The design and control of a two-armed, cooperating, flexible-drivetrain robot system. [D] . Pfeffer, Lawrence E. 1994

机译：两臂协作的灵活传动系统机器人系统的设计和控制。
6. Flexible trial design in practice - stopping arms for lack-of-benefit and adding research arms mid-trial in STAMPEDE: a multi-arm multi-stage randomized controlled trial [O] . Matthew R Sydes, Mahesh KB Parmar, Malcolm D Mason, 2012

机译：实践中灵活的试验设计-在STAMPEDE中停止缺乏治疗的武器并在中期试验中添加研究武器：多臂多阶段随机对照试验
7. Force Sensorless Control in a Flexible Link Arm Based on Estimated Reaction Torque. [O] . Masaaki Shibata, Kenichi Isomura, Toshiyuki Murakami, 1997

机译：基于估计的反作用扭矩，在柔性连杆臂中强制无传感器控制。
8. Design of a three-axis attitude control system for a spacecraft acted upon by random perturbations Final report [R] . Friedland, B., Sarachik, P. E., Thau, F. E. 1968

机译：用随机扰动作用的航天器三轴姿态控制系统的设计最终报告

Reaction Control System Design for Unsymmetric Flexible Spacecraft with Consideration of Torque Arm Perturbation

摘要

著录项

相似文献

相关主题

期刊订阅