Adaptive output feedback tracking control of multiple spacecraft

H. Wong, Vikram Kapila, A. Sparks

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

Abstract

In this paper, an adaptive, output feedback control design methodology is presented for a multiple spacecraft formation flying (MSFF) system. A Lagrangian derivation of the MSFF model is considered to produce position dynamics for follower spacecraft #n relative to follower spacecraft #(n - 1), assuming that the leader spacecraft in the formation follows a no-thrust, natural, elliptical orbit. Next, a control law is designed to provide a filtered velocity measurement and a desired adaptive compensation with semi-global, asymptotic, relative position tracking. The proposed control law is simulated for the case of two and three spacecraft and is shown to yield semi-global, asymptotic tracking of the relative position errors.

Original languageEnglish (US)
Title of host publicationProceedings of the American Control Conference
Pages698-703
Number of pages6
Volume2
StatePublished - 2001
Event2001 American Control Conference - Arlington, VA, United States
Duration: Jun 25 2001Jun 27 2001

Other

Other2001 American Control Conference
CountryUnited States
CityArlington, VA
Period6/25/016/27/01

Fingerprint

Spacecraft
Feedback
Velocity measurement
Feedback control
Orbits

ASJC Scopus subject areas

  • Control and Systems Engineering

Cite this

Wong, H., Kapila, V., & Sparks, A. (2001). Adaptive output feedback tracking control of multiple spacecraft. In Proceedings of the American Control Conference (Vol. 2, pp. 698-703)

Adaptive output feedback tracking control of multiple spacecraft. / Wong, H.; Kapila, Vikram; Sparks, A.

Proceedings of the American Control Conference. Vol. 2 2001. p. 698-703.

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

Wong, H, Kapila, V & Sparks, A 2001, Adaptive output feedback tracking control of multiple spacecraft. in Proceedings of the American Control Conference. vol. 2, pp. 698-703, 2001 American Control Conference, Arlington, VA, United States, 6/25/01.
Wong H, Kapila V, Sparks A. Adaptive output feedback tracking control of multiple spacecraft. In Proceedings of the American Control Conference. Vol. 2. 2001. p. 698-703
Wong, H. ; Kapila, Vikram ; Sparks, A. / Adaptive output feedback tracking control of multiple spacecraft. Proceedings of the American Control Conference. Vol. 2 2001. pp. 698-703
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