Composite Adaptive Orbit Control and Parameter Estimation by Integral Excitation Around Asteroids
2023; American Institute of Aeronautics and Astronautics; Volume: 46; Issue: 9 Linguagem: Inglês
10.2514/1.g007270
ISSN1533-3884
AutoresKeum W. Lee, Sahjendra N. Singh,
Tópico(s)Stellar, planetary, and galactic studies
ResumoNo AccessEngineering NotesComposite Adaptive Orbit Control and Parameter Estimation by Integral Excitation Around AsteroidsKeum W. Lee and Sahjendra N. SinghKeum W. LeeCatholic Kwandong University, Gangwon 25601, Republic of Korea and Sahjendra N. SinghUniversity of Nevada Las Vegas, Las Vegas, Nevada 89154-4026Published Online:21 May 2023https://doi.org/10.2514/1.G007270SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Werner R. A. and Scheeres D. J., "Exterior Gravitation of a Polyhedron Derived and Compared with Harmonic and Mascon Gravitation Representations of Asteroid 4769 Castalia," Celestial Mechanics and Dynamical Astronomy, Vol. 65, No. 3, 1996, pp. 313–344. https://doi.org/10.1007/BF00053511 Google Scholar[2] Herrera-Sucarrat E., Palmer P. L. and Roberts R. 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LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byAdaptive Spacecraft Attitude Control and Asteroid Parameter Estimation4 August 2023 What's Popular Volume 46, Number 9September 2023 CrossmarkInformationCopyright © 2023 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3884 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. KeywordsAsteroid-orbiting spacecraftcomposite identifiercomposite adaptive orbit control Integral regressor excitationGradient-based adaptation lawLyapunov stabilityNonlinear systemsPDF Received29 September 2022Accepted16 April 2023Published online21 May 2023
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