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2018 | OriginalPaper | Chapter

2. Modeling and Hardware Components of Control System of the OTV

Authors : Xuefeng Li, Chaobing Li

Published in: Navigation and Guidance of Orbital Transfer Vehicle

Publisher: Springer Singapore

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Abstract

The design of navigation and guidance system of the OTV is carried out on the basis of the kinetic equations and dynamic equations of the control object.

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Literature
1.
go back to reference Li Xuefeng, Wang Qing. 2014. Design and Verification of Flight Control System of Launch Vehicle. National Defense Industry Press. Li Xuefeng, Wang Qing. 2014. Design and Verification of Flight Control System of Launch Vehicle. National Defense Industry Press.
2.
go back to reference Liu Haiying, Wang Huinan, Chen Zhiming. 2013. Principle and Application of GNSS Navigation. National Defense Industry Press. Liu Haiying, Wang Huinan, Chen Zhiming. 2013. Principle and Application of GNSS Navigation. National Defense Industry Press.
3.
go back to reference Fang Jiancheng, Ning Xiaolin. 2006. Principle and Application of Celestial Navigation. Beihang University Press. Fang Jiancheng, Ning Xiaolin. 2006. Principle and Application of Celestial Navigation. Beihang University Press.
4.
go back to reference Xia Kang. 2013. Research on Hardware Fault Tolerance Technology of High Reliable Parallel Space-borne Computer. Shanghai Jiao Tong University. Xia Kang. 2013. Research on Hardware Fault Tolerance Technology of High Reliable Parallel Space-borne Computer. Shanghai Jiao Tong University.
5.
go back to reference Bing, Shan, and Miu Dong. 2004. Design and Optimization of Redundancy of Strapdown Inertial Measurement Unit. Missiles and Space Vehicles 3: 25–29. Bing, Shan, and Miu Dong. 2004. Design and Optimization of Redundancy of Strapdown Inertial Measurement Unit. Missiles and Space Vehicles 3: 25–29.
6.
go back to reference Mingqiao, Yue, and Wang Tanquan. 2005. The Analysis and Developing Trends of Laser Gyroscope. Winged Missiles Journal 12: 46–48. Mingqiao, Yue, and Wang Tanquan. 2005. The Analysis and Developing Trends of Laser Gyroscope. Winged Missiles Journal 12: 46–48.
7.
go back to reference Shiqin, Zhou. 2001. Development of New Inertial Technology. Winged Missile Journal 6: 70–77. Shiqin, Zhou. 2001. Development of New Inertial Technology. Winged Missile Journal 6: 70–77.
8.
go back to reference Qin Yongyuan. 2006. Inertial Technology. Science Press. Qin Yongyuan. 2006. Inertial Technology. Science Press.
9.
go back to reference Lu Xinzhi. 2013. Research on Deep Coupling Technique of GNSS Receiver and Inertial Navigation. University of Electronic Science and Technology. Lu Xinzhi. 2013. Research on Deep Coupling Technique of GNSS Receiver and Inertial Navigation. University of Electronic Science and Technology.
10.
go back to reference Hui, Zhang. 2005. Star Sensor. Journal of Hechi University 4: 54–56. Hui, Zhang. 2005. Star Sensor. Journal of Hechi University 4: 54–56.
11.
go back to reference Otiver Montenbruck, Eberhard Gill. 2012. Methods and Application of Satellite Orbital Model. Translated by Wang Jiasong, Zhu Kaijian, Hu Xiaogong. Beijing: National Defense Industry Press. Otiver Montenbruck, Eberhard Gill. 2012. Methods and Application of Satellite Orbital Model. Translated by Wang Jiasong, Zhu Kaijian, Hu Xiaogong. Beijing: National Defense Industry Press.
12.
go back to reference Wang Wei, Yu Zhijian. 2007. Orbital Determination of Flight Vehicle: Model and Algorithm. National Defense Industry Press. Wang Wei, Yu Zhijian. 2007. Orbital Determination of Flight Vehicle: Model and Algorithm. National Defense Industry Press.
13.
go back to reference Zhang Libin. 2010. Research on Navigation, Midcourse Correction and Attitude Control of Rocket Upper Stage. Harbin Institute of Technology. Zhang Libin. 2010. Research on Navigation, Midcourse Correction and Attitude Control of Rocket Upper Stage. Harbin Institute of Technology.
14.
go back to reference Yu Yongjiang. 2009. Research on Upper Stage Guidance Method. Harbin Institute of Technology. Yu Yongjiang. 2009. Research on Upper Stage Guidance Method. Harbin Institute of Technology.
15.
go back to reference Yang Jiachi, Fan Qinhong, Zhang Yuntong, Yang Weikang, Chen Shuqing. 1999. Orbital Dynamics and Control of Flight Vehicle: First Volume. China Astronautic Publishing House. Yang Jiachi, Fan Qinhong, Zhang Yuntong, Yang Weikang, Chen Shuqing. 1999. Orbital Dynamics and Control of Flight Vehicle: First Volume. China Astronautic Publishing House.
16.
go back to reference Zhang Renwei. 1998. Attitude Dynamics and Control of Satellite Orbit. Beihang University Press. Zhang Renwei. 1998. Attitude Dynamics and Control of Satellite Orbit. Beihang University Press.
Metadata
Title
Modeling and Hardware Components of Control System of the OTV
Authors
Xuefeng Li
Chaobing Li
Copyright Year
2018
Publisher
Springer Singapore
DOI
https://doi.org/10.1007/978-981-10-6334-3_2

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