Multistepping approach to finite-interval missile integrated control
- Author
- VADDI, S. S1 ; MENON, P. K1 ; SWERIDUK, G. D1 ; OHLMEYER, E. J2
[1] Optimal Synthesis, Inc, Palo Alto, California 94303, United States
[2] Naval Surface Warfare Center, Dahlgreen, Virginia 22448, United States - Source
Journal of guidance, control, and dynamics. 2006, Vol 29, Num 4, pp 1015-1018, 4 p ; ref : 7 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)
- Calcul ensembliste Commande missile
- Keyword (en)
- Set computation Missile control
- Keyword (es)
- Calcúlo conjunto
- Classification
- 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
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 17958342
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
10.2514/1.19956 
https://dx.doi.org/10.2514/1.19956
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