Application of adaptive fuzzy slide model control in reconfigurable flight controller

Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica

Volumn 23, Issue 6, 2002, Pages 538-541

  Hu, Meng Quan ^a   Wang, Jian Pei ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Adaptive fuzzy system; Nonlinear dynamic inversion; Reconfiguration; Slide model control; Vectored thrust

Indexed keywords

ALGORITHMS; CALCULATIONS; RELIABILITY;

AMBIGUITY SCREEN; DECORRELATION PROCESS; ORDERING PROCESS; ORDERING SCREEN DECORRELATION;

GLOBAL POSITIONING SYSTEM;

EID: 0038199831     PISSN: 10006893     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (5)

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2. Kim B S, Calise A J. Nonlinear fight control using neural networks [J]. Journal of Guidance, control and Dynamics, 1997, 20(1): 26-33.
3. Wang L X. Adaptive fuzzy system and control-design and stability analysis [M]. Beijing: National Defense Industry Press, 1995. 27-34.
4. Bugajski D J, Enns D F. Nonlinear control law with application to high angle-of-attack flight [J]. Journal of Guidance, Control and Dynamics, 1992, 15(3): 761-767.
5. Slotine J J E, Li W P. Applied nonlinear control [M]. Beijing: National Defense Industry Press, 1992. 174-192.