国外航天器高精度高稳定度高敏捷指向技术综述
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摘要
调研了国外航天器高精度高稳定度高敏捷指向技术发展现状,分析了其实现的主要技术途径,研究表明高精度高稳定度高敏捷指向作为一项系统性技术,需要从构型布局、结构动力学、控制等多方面开展综合分析与设计。文章对其中一体化构型布局设计、微振动抑制、多级复合控制和大力矩执行机构等关键技术进行了总结和分析,可为我国高性能航天器的发展提供借鉴。
In this paper,the development of high accuracy,high stability and high agility pointing technology of spacecraft is introduced.The main methods that achieve the above performance are analyzed.The research shows that as a systematic technology,high accuracy,high stability and high agility pointing should be achieved by complex analysis and design considering all these composite factors of configuration,structural dynamics and control.Some key technologies such as integrated configuration design,micro vibration suppression,multi-stage complex control,actuators with large torque are summarized,which can provide a reference for the future development of spacecrafts of China with high performance.
In this paper,the development of high accuracy,high stability and high agility pointing technology of spacecraft is introduced.The main methods that achieve the above performance are analyzed.The research shows that as a systematic technology,high accuracy,high stability and high agility pointing should be achieved by complex analysis and design considering all these composite factors of configuration,structural dynamics and control.Some key technologies such as integrated configuration design,micro vibration suppression,multi-stage complex control,actuators with large torque are summarized,which can provide a reference for the future development of spacecrafts of China with high performance.
引文
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[4]Luis Meza,Frank Tung,Satya Anandakrishnan,et al.Line of sight stabilization of James Webb Space Telescope[C]//27th Annual AAS Guidance and Control Conference.San Diego,CA:AAS,2005
[5]Yevgeny S,Houria S,Vivtor F.Precise nonius guidance and image stabilization of a large space telescope[C]//2011 5th International Conference on Recent Advances in Space Technologies.Istanbul:RAST,2011:869-874
[6]Brugarolas P,Alexander J,Tmugor J,et a1.ACCESS pointing control system[C]//Space Telescopes and Instrumentation:Optical,Infrared,and Millimeter Wave.Bellingham:SPIE,2010
[7]Phillip Vallone,Robert M Egerman.Active dynamic isolation and pointing control system design and analysis for the ACCESS TPF mission concept[C]//Proceeding of SPIE Symposium on SPIE Astronomical Telescopes and Instrumentation.Bellingham:SPIE,2010
[8]John Trauger.ACCESS:a NASA mission concept study of anactively corrected coronagraph for Exoplanet System Studies[C]//In Proceeding of SPIE.Bellingham:SPIE,2008
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[12]Satellite Imaging Corp.Pleiades-1Bsatellite imagery and satellite sensor specification[EB/OL].[2016-09-26].http://www.satimagingcorp.com/satellite-sensors/Pleiades-1b/
[13]H Ansari.Digital control design of a CCD-based tracking loop for precision beam pointing[C]//Proceedings of SPIE-The International Society for Optical Engineering.Bellingham:SPIE,1994
[14]Nelson Pedreiro.Spacecraft architecture for Disturbance-Free Payload[C]//AIAA:Guidance,Navigation,and Control Conference and Exhibit.Washington D.C.:AIAA,2002