Skip to main content
Top

2018 | OriginalPaper | Chapter

8. Guidance and Midcourse Correction Technology

Authors : Xuefeng Li, Chaobing Li

Published in: Navigation and Guidance of Orbital Transfer Vehicle

Publisher: Springer Singapore

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

The orbit of Orbital Transfer Vehicle (OTV) commonly consists of the active flight section and free flight section. Among which, the active flight section refers to the motional process of the flight vehicle under the ignition of orbit maneuver motor. The free flight section is the motional process of the flight vehicle under the actions of gravitation and various types of perturbation effects after the shutdown of orbit maneuver motor.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

Literature
1.
go back to reference Song, Zhengyu. 2014. Design of Control System of High Reliability Launch Vehicle. China Astronautic Publishing House. Song, Zhengyu. 2014. Design of Control System of High Reliability Launch Vehicle. China Astronautic Publishing House.
2.
go back to reference Zhang, Libing. 2010. Rocket Upper Stage Navigation, Research on Midcourse Correction and Attitude Control. Harbin Institute of Technology. Zhang, Libing. 2010. Rocket Upper Stage Navigation, Research on Midcourse Correction and Attitude Control. Harbin Institute of Technology.
3.
go back to reference Zeng, Guoqiang. 2000. Research on Dynamic of Orbits and Guidance Methods of Lunar Probe. National University of Defense Technology. Zeng, Guoqiang. 2000. Research on Dynamic of Orbits and Guidance Methods of Lunar Probe. National University of Defense Technology.
4.
go back to reference Yuan, Jianping, Yushan Zhao. 2014. Design of Flight Vehicle Deep Space Flight Trajectory. China Astronautic Publishing House. Yuan, Jianping, Yushan Zhao. 2014. Design of Flight Vehicle Deep Space Flight Trajectory. China Astronautic Publishing House.
5.
go back to reference Cui, Pingyuan, Dong Qiao, Gutao Cui. 2013. Design and Optimization of Deep Space Exploration Orbit. Science Press. Cui, Pingyuan, Dong Qiao, Gutao Cui. 2013. Design and Optimization of Deep Space Exploration Orbit. Science Press.
6.
go back to reference Lu, P., S. Forbes, and M. Baldwin. 2012. A Versatile Powered Guidance Algorithm. In AIAA Guidance, Navigation, and Control Conference, 4843. Lu, P., S. Forbes, and M. Baldwin. 2012. A Versatile Powered Guidance Algorithm. In AIAA Guidance, Navigation, and Control Conference, 4843.
7.
go back to reference Yang, Jiachi, Qinhong Fang, Yuntong Zhong, Weilian Yang, Shuqing Chen. 1999. Dynamics of Orbits and Control of Aircraft: (First Volume). China Astronautic Publishing House. Yang, Jiachi, Qinhong Fang, Yuntong Zhong, Weilian Yang, Shuqing Chen. 1999. Dynamics of Orbits and Control of Aircraft: (First Volume). China Astronautic Publishing House.
8.
go back to reference Yang, Jiachi, Qinghong Fan, Yuntong Zhang. 2001. Dynamics of Orbits and Control of Aircraft: (Second Volume). China Astronautic Publishing House. Yang, Jiachi, Qinghong Fan, Yuntong Zhang. 2001. Dynamics of Orbits and Control of Aircraft: (Second Volume). China Astronautic Publishing House.
9.
go back to reference Zhang, Renwei. 1998. Dynamics of Attitude and Control of Satellite Orbit. Beihang University Press. Zhang, Renwei. 1998. Dynamics of Attitude and Control of Satellite Orbit. Beihang University Press.
10.
go back to reference Wang, Mengyi, Yong Jiang. 2008. Research on Midcourse Correction of Transfer Track for Near-Ground Vehicle . In 2008 Proceedings of The National Doctoral Forum 2008 (Aeronautical and Astronautical Science and Technology, 312–323. Wang, Mengyi, Yong Jiang. 2008. Research on Midcourse Correction of Transfer Track for Near-Ground Vehicle . In 2008 Proceedings of The National Doctoral Forum 2008 (Aeronautical and Astronautical Science and Technology, 312–323.
11.
Metadata
Title
Guidance and Midcourse Correction Technology
Authors
Xuefeng Li
Chaobing Li
Copyright Year
2018
Publisher
Springer Singapore
DOI
https://doi.org/10.1007/978-981-10-6334-3_8

Premium Partner