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Integrated estimation/guidance design approach for improved homing against randomly maneuvering targets

Author
SHINAR, Josef1 ; TURETSKY, Vladimir1 ; OSHMAN, Yaakov1
[1] Technion-Israel Institute of Technology, Haifa 32000, Israel
Source

Journal of guidance, control, and dynamics. 2007, Vol 30, Num 1, pp 154-161, 8 p ; ref : 34 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)
Aéronef Conception intégrée Erreur estimation Estimation erreur Guidage missile Interception Manoeuvrabilité Missile Méthode Monte Carlo Poursuite cible
Keyword (en)
Aircraft Integrated design Estimation error Error estimation Missile guidance Interception Maneuverability Missile Monte Carlo method Target tracking
Keyword (es)
Aeronave Concepción integrada Error estimación Estimación error Intercepción Maniobrabilidad Misil Método Monte Carlo
Classification
Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D02 Computer science; control theory; systems / 001D02D Control theory. Systems / 001D02D11 Robotics

Pascal
001 Exact sciences and technology / 001D Applied sciences / 001D12 Mechanical engineering. Machine design / 001D12A General

Discipline
Computer science : theoretical automation and systems Mechanical engineering. Mechanical construction. Handling
Origin
Inist-CNRS
Database
PASCAL
INIST identifier
18473880

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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