A nonlinear helicopter tracker using attitude measurements
- Author
- ANDRISANI, D. II; EUNG TAI KIM; SCHIERMAN, J; KUHL, F. P
Purdue univ., school aeronautics astronautics, West Lafayette IN 47907, United States - Source
IEEE transactions on aerospace and electronic systems. 1991, Vol 27, Num 1, pp 40-47 ; ref : 9 ref
- CODEN
- IEARAX
- ISSN
- 0018-9251
- Scientific domain
- Aeronautics astronautics; Electronics; Telecommunications
- Publisher
- Institute of Electrical and Electronics Engineers, New York, NY
- Publication country
- United States
- Document type
- Article
- Language
- English
- Keyword (fr)
- Filtre Kalman Hélicoptère Mesure Performance Radar Simulation Système non linéaire
- Keyword (en)
- Kalman filter Helicopter Measurement Performance Radar Simulation Non linear system
- Keyword (es)
- Filtro Kalman Helicóptero Medida Rendimiento Radar Simulación Sistema no lineal
- Classification
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D04 Telecommunications and information theory / 001D04A Information, signal and communications theory
- Discipline
- Telecommunications and information theory
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 5206875
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
10.1109/7.68146 
https://dx.doi.org/10.1109/7.68146
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