Analysis and control of satellite orbits around oblate earth using perturbation method

Qiguo Yan, Vikram Kapila

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this paper, we develop the dynamics of a particle satellite motion around the oblate earth using a special rotating reference frame. This dynamics is used to deduce the conditions under which the orbital plane of motion of the particle satellite remains fixed. Next, a two-scale perturbation analysis is performed to seek the analytical solution of the particle satellite motion in the presence of the J2 influence of the oblate earth. The resulting analytical solution of the planar dynamics of the particle satellite is utilized to produce a planar motion controller so that the perturbation forces in the radial direction are tailored to guarantee that the particle satellite moves in a periodic trajectory. Finally, illustrative simulations are provided to demonstrate the effectiveness of the proposed framework.

Original languageEnglish (US)
Title of host publicationProceedings of the IEEE Conference on Decision and Control
Pages1517-1522
Number of pages6
Volume2
StatePublished - 2001
Event40th IEEE Conference on Decision and Control (CDC) - Orlando, FL, United States
Duration: Dec 4 2001Dec 7 2001

Other

Other40th IEEE Conference on Decision and Control (CDC)
CountryUnited States
CityOrlando, FL
Period12/4/0112/7/01

Fingerprint

Orbits
Earth (planet)
Satellites
Trajectories
Controllers

ASJC Scopus subject areas

  • Chemical Health and Safety
  • Control and Systems Engineering
  • Safety, Risk, Reliability and Quality

Cite this

Yan, Q., & Kapila, V. (2001). Analysis and control of satellite orbits around oblate earth using perturbation method. In Proceedings of the IEEE Conference on Decision and Control (Vol. 2, pp. 1517-1522)

Analysis and control of satellite orbits around oblate earth using perturbation method. / Yan, Qiguo; Kapila, Vikram.

Proceedings of the IEEE Conference on Decision and Control. Vol. 2 2001. p. 1517-1522.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Yan, Q & Kapila, V 2001, Analysis and control of satellite orbits around oblate earth using perturbation method. in Proceedings of the IEEE Conference on Decision and Control. vol. 2, pp. 1517-1522, 40th IEEE Conference on Decision and Control (CDC), Orlando, FL, United States, 12/4/01.
Yan Q, Kapila V. Analysis and control of satellite orbits around oblate earth using perturbation method. In Proceedings of the IEEE Conference on Decision and Control. Vol. 2. 2001. p. 1517-1522
Yan, Qiguo ; Kapila, Vikram. / Analysis and control of satellite orbits around oblate earth using perturbation method. Proceedings of the IEEE Conference on Decision and Control. Vol. 2 2001. pp. 1517-1522
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