Control of formation flight via extremum seeking

Proceedings of the American Control Conference

Volumn 4, Issue , 2002, Pages 2848-2853

  Binetti, Paolo ^a   Ariyur, Kartik B ^b   Krstić, Miroslav ^b   Bernelli, Franco ^a  

^a POLITECNICO DI MILANO   (Italy)

^b UNIVERSITY OF CALIFORNIA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; CLOSED LOOP CONTROL SYSTEMS; CONTROL NONLINEARITIES; FEEDBACK CONTROL; FLIGHT DYNAMICS; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; WAKES;

AERODYNAMIC INTERFERENCE; EXTREMUM SEEKING; FORMATION FLIGHT CONTROL;

CONTROL SYSTEM SYNTHESIS;

EID: 0036059712     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2002.1025221     Document Type: Article

References (10)

1. Analysis and design of multivariable extremum seeking
2. Design performance and modeling considerations for closed formation flight
3. Peak-seeking control with application to formation flight
4. Measurement of the wake characteristics of the Boeing 747, Lockheed C-5A, and other aircraft
5. Autonomous formation flight
6. Aircraft wake vortices: A state of the art review of the United States R&D program
7. Aircraft handling qualities data
8. The use of aircraft wakes to achieve power reduction in formation flight
9. Tight formation flight control
10. C-5 modernization-step by step