单框架控制力矩陀螺修正奇异方向操纵律
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- 英文论文题名：Modified Singular Direction Steering Logic for Single Gimbal Control Moment Gyroscopes
- 论文作者：吴云华 ; 韩锋 ; 华冰 ; 陈志明 ; 徐大富 ; 郁丰
- 英文论文作者：Yun-Hua Wu ; Feng Han ; Bing Hua ; Zhi-Ming Chen ; Da-Fu Xu ; Feng Yu ; School of Astronautics ; Nanjing University of Aeronautics and Astronautics ; Aerospace System Engineering Shanghai
- 年：2017
- 作者机构：南京航空航天大学航天学院;上海宇航系统工程研究所;
- 论文关键词：敏捷卫星 ; 单框架控制力矩陀螺 ; 甲烷构型 ; 修正操纵律
- 英文论文关键词：Agile satellite ; SGCMG ; Methane configuration ; Modified steering logic
- 会议召开时间：2017-07-26
- 会议录名称：第36届中国控制会议论文集（A）
- 英文会议录名称：Proceedings of the 36th Chinese Control Conference（A）
- 语种：中文
- 分类号：V448.22
- 学会代码：KZLL
- 会议名称：第36届中国控制会议
- 会议地点：中国辽宁大连
- 主办单位：中国自动化学会控制理论专业委员会
- 学会名称：中国自动化学会控制理论专业委员会
- 页数：6
- 文件大小：980k
- 原文格式：D
- 会议级别：全国
摘要
针对以单框架控制力矩陀螺系统为执行机构的敏捷航天器姿态控制问题,提出了控制力矩陀螺修正的奇异方向操纵律。在奇异值分解的基础上,应用叉乘运算使得雅可比矩阵始终处于满秩状态,从而实现对奇异方向操纵律的修正。分析表明,该操纵律与基于伪逆的操控律相比,操作简单,适用于各种单框架控制力矩陀螺构型。该操纵律能够有效避免控制力矩陀螺系统陷入奇异。本文的研究成果可用于敏捷航天器在轨实时姿态控制。
This paper focus on problem of agile satellite attitude control using Single Gimbal Control Moment Gyroscope(SGCMG) problem as attitude control actuator. The modified singular direction steering logic is proposed for CMG control.Based on the Singular Value Decomposition(SVD) method, the cross product technique is applied to guarantee the full rank of Jacobian matrix and the singular direction can be avoided. The theoretical analysis suggests the simplicity in operation and universality for all CMG configurations compared to the pseudo-inverse-based steering logic. The proposed modified logic can help the CMG cluster to escape the singularity. The research of this paper is qualified for real time on orbit application for agile satellite attitude maneuvering.
This paper focus on problem of agile satellite attitude control using Single Gimbal Control Moment Gyroscope(SGCMG) problem as attitude control actuator. The modified singular direction steering logic is proposed for CMG control.Based on the Singular Value Decomposition(SVD) method, the cross product technique is applied to guarantee the full rank of Jacobian matrix and the singular direction can be avoided. The theoretical analysis suggests the simplicity in operation and universality for all CMG configurations compared to the pseudo-inverse-based steering logic. The proposed modified logic can help the CMG cluster to escape the singularity. The research of this paper is qualified for real time on orbit application for agile satellite attitude maneuvering.
引文
[1]K.Takada,H.Kojima,N.Matsuda,Control Moment Gyro Singularity-Avoidance Steering Control Based on Singular-Surface Cost Function.Journal of Guidance,Control,and Dynamics,(33)5:1442-1450,2010
[2]T.Kanzawa,M.Haruki,Yamanaka K,Steering Law of Control Moment Gyroscopes for Agile Attitude Maneuvers.Journal of Guidance,Control,and Dynamics,(39)4:952-962,2016.
[3]B.Wie,D.Bailey,C.Heiberg,Robust CMG Steering Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros.Journal of Guidance,Control,and Dynamics,25(4):865-872,2001.
[4]J.Laura,P.Mason P,A Generalized Framework for Linearly-Constrained Singularity-Free Control Moment Gyro Steering Laws.AIAA Guidance,Navigation,and Control Conference.2009:1-10.
[5]B.Wie,W.New Singularity Escape/Avoidance Steering Logic for Control Moment Gyro Systems.AIAA Guidance,Navigation,and Control Conference and Exhibit.2003:1-9.
[6]T.Ozan,Momentum Envelopes and Steering of Control Moment Gyroscope Clusters.AIAA/AAS Astrodynamics Specialist Conference.2012.
[7]B.Wie,Singularity Escape/Avoidance Steering Logic for Control Moment Gyro Systems.Journal of Guidance,Control,and Dynamics,28(5):948-956,2005.
[8]B.Girouart,I.Sebbag,J.M.Lachiver,Performance of Pleiades-HR Agile Attitude Control System.Proceeding of the 5th International ESA Conference on Spacecraft Guidance,Navigation and Control System.2002.
[9]V.Lappas,B.Wie,Robust CMG Steering Logic with Gimbal Angle Constraints,AIAA Paper,2006:1-15.
[10]T.Meng,S.Matunaga,Modified Singular-Direction Avoidance Steering for Control Moment Gyros.Journal of Guidance,Control,and Dynamics,(34)6:1915-1920,2011.
[11]A.Sajjad P.L.Palmer,M.Roberts,Exact Steering Law for Pyramid-type Four Control Moment Gyro Systems.AIAA/AAS Astrodynamics Specialist Conference and Exhibit.2006:1-10.
[12]Kurokawa H.Survey of Theory and Steering Laws of Single-Gimbal Control Moment Gyros.Journal of Guidance,Control,and Dynamics,30(5):1331-1340,2007.
[13]K.Yamada T.Asai,I.Jikuya,Inverse Kinematics in Pyramid-Type Single-Gimbal Control Moment Gyro System.Journal of Guidance,Control,and Dynamics,39(8):1897-1907,2016
[2]T.Kanzawa,M.Haruki,Yamanaka K,Steering Law of Control Moment Gyroscopes for Agile Attitude Maneuvers.Journal of Guidance,Control,and Dynamics,(39)4:952-962,2016.
[3]B.Wie,D.Bailey,C.Heiberg,Robust CMG Steering Robust Steering Logic for Redundant Single-Gimbal Control Moment Gyros.Journal of Guidance,Control,and Dynamics,25(4):865-872,2001.
[4]J.Laura,P.Mason P,A Generalized Framework for Linearly-Constrained Singularity-Free Control Moment Gyro Steering Laws.AIAA Guidance,Navigation,and Control Conference.2009:1-10.
[5]B.Wie,W.New Singularity Escape/Avoidance Steering Logic for Control Moment Gyro Systems.AIAA Guidance,Navigation,and Control Conference and Exhibit.2003:1-9.
[6]T.Ozan,Momentum Envelopes and Steering of Control Moment Gyroscope Clusters.AIAA/AAS Astrodynamics Specialist Conference.2012.
[7]B.Wie,Singularity Escape/Avoidance Steering Logic for Control Moment Gyro Systems.Journal of Guidance,Control,and Dynamics,28(5):948-956,2005.
[8]B.Girouart,I.Sebbag,J.M.Lachiver,Performance of Pleiades-HR Agile Attitude Control System.Proceeding of the 5th International ESA Conference on Spacecraft Guidance,Navigation and Control System.2002.
[9]V.Lappas,B.Wie,Robust CMG Steering Logic with Gimbal Angle Constraints,AIAA Paper,2006:1-15.
[10]T.Meng,S.Matunaga,Modified Singular-Direction Avoidance Steering for Control Moment Gyros.Journal of Guidance,Control,and Dynamics,(34)6:1915-1920,2011.
[11]A.Sajjad P.L.Palmer,M.Roberts,Exact Steering Law for Pyramid-type Four Control Moment Gyro Systems.AIAA/AAS Astrodynamics Specialist Conference and Exhibit.2006:1-10.
[12]Kurokawa H.Survey of Theory and Steering Laws of Single-Gimbal Control Moment Gyros.Journal of Guidance,Control,and Dynamics,30(5):1331-1340,2007.
[13]K.Yamada T.Asai,I.Jikuya,Inverse Kinematics in Pyramid-Type Single-Gimbal Control Moment Gyro System.Journal of Guidance,Control,and Dynamics,39(8):1897-1907,2016