Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point

Hong Wong, Vikram Kapila

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

Abstract

In this paper, an adaptive control algorithm is presented to enable a spacecraft to track desired trajectories near the L2 Lagrange point in the Sun-Earth system. An adaptive full-state feedback control law, designed using a Lyapunov-type analysis, exhibits globally asymptotic position tracking in the presence of the unknown spacecraft mass. The control law is simulated for a Lyapunov orbit in the vicinity of the L2 Lagrange point as the periodic reference trajectory.

Original languageEnglish (US)
Title of host publicationProceedings of the American Control Conference
Pages1116-1121
Number of pages6
Volume2
StatePublished - 2003
Event2003 American Control Conference - Denver, CO, United States
Duration: Jun 4 2003Jun 6 2003

Other

Other2003 American Control Conference
CountryUnited States
CityDenver, CO
Period6/4/036/6/03

Fingerprint

Sun
Spacecraft
Earth (planet)
Trajectories
State feedback
Feedback control
Orbits

ASJC Scopus subject areas

  • Control and Systems Engineering

Cite this

Wong, H., & Kapila, V. (2003). Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point. In Proceedings of the American Control Conference (Vol. 2, pp. 1116-1121)

Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point. / Wong, Hong; Kapila, Vikram.

Proceedings of the American Control Conference. Vol. 2 2003. p. 1116-1121.

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

Wong, H & Kapila, V 2003, Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point. in Proceedings of the American Control Conference. vol. 2, pp. 1116-1121, 2003 American Control Conference, Denver, CO, United States, 6/4/03.
Wong H, Kapila V. Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point. In Proceedings of the American Control Conference. Vol. 2. 2003. p. 1116-1121
Wong, Hong ; Kapila, Vikram. / Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point. Proceedings of the American Control Conference. Vol. 2 2003. pp. 1116-1121
@inproceedings{9eaa1887a3434ac68992fb96077b76b1,
title = "Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point",
abstract = "In this paper, an adaptive control algorithm is presented to enable a spacecraft to track desired trajectories near the L2 Lagrange point in the Sun-Earth system. An adaptive full-state feedback control law, designed using a Lyapunov-type analysis, exhibits globally asymptotic position tracking in the presence of the unknown spacecraft mass. The control law is simulated for a Lyapunov orbit in the vicinity of the L2 Lagrange point as the periodic reference trajectory.",
author = "Hong Wong and Vikram Kapila",
year = "2003",
language = "English (US)",
volume = "2",
pages = "1116--1121",
booktitle = "Proceedings of the American Control Conference",

}

TY - GEN

T1 - Adaptive Nonlinear Control of Spacecraft Near Sun-Earth L2 Lagrange Point

AU - Wong, Hong

AU - Kapila, Vikram

PY - 2003

Y1 - 2003

N2 - In this paper, an adaptive control algorithm is presented to enable a spacecraft to track desired trajectories near the L2 Lagrange point in the Sun-Earth system. An adaptive full-state feedback control law, designed using a Lyapunov-type analysis, exhibits globally asymptotic position tracking in the presence of the unknown spacecraft mass. The control law is simulated for a Lyapunov orbit in the vicinity of the L2 Lagrange point as the periodic reference trajectory.

AB - In this paper, an adaptive control algorithm is presented to enable a spacecraft to track desired trajectories near the L2 Lagrange point in the Sun-Earth system. An adaptive full-state feedback control law, designed using a Lyapunov-type analysis, exhibits globally asymptotic position tracking in the presence of the unknown spacecraft mass. The control law is simulated for a Lyapunov orbit in the vicinity of the L2 Lagrange point as the periodic reference trajectory.

UR - http://www.scopus.com/inward/record.url?scp=0142169398&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0142169398&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:0142169398

VL - 2

SP - 1116

EP - 1121

BT - Proceedings of the American Control Conference

ER -