Energy suboptimal collision-free reconfiguration for spacecraft formation flying
- Author
- SULTAN, Cornel1 ; SEERERAM, Sanjeev2 ; MEHRA, Raman K2
[1] United Technologies Research Center, East Hartford, Connecticut 06108, United States
[2] Scientific Systems Corporation, Inc, Woburn, Massachusetts 01801, United States - Source
Journal of guidance, control, and dynamics. 2006, Vol 29, Num 1, pp 190-192, 3 p ; ref : 4 ref
- CODEN
- JGCODS
- ISSN
- 0731-5090
- Scientific domain
- Aeronautics astronautics; Control theory, operational research; Mechanics acoustics; Transportation
- Publisher
- American Institute of Aeronautics and Astronautics, Reston, VA
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Energie libre Esquive collision Formation Reconfiguration Spationef
- Keyword (en)
- Free energy Collision avoidance Formation Reconfiguration Spacecraft
- Keyword (es)
- Energía libre Esquiva colisión Formación Reconfiguración Vehículo espacial
- Classification
- Pascal
- 001 Exact sciences and technology / 001B Physics / 001B40 Fundamental areas of phenomenology (including applications) / 001B40F Solid mechanics / 001B40F10 Solid dynamics (ballistics, collision, multibody system, stabilization...)
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D02 Computer science; control theory; systems / 001D02D Control theory. Systems
- Discipline
- Computer science : theoretical automation and systems Physics : solid mechanics
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 17439966
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.2514/1.10781 
https://dx.doi.org/10.2514/1.10781
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