A study on the optimal flight control for an autonomous UAV

2006 IEEE International Conference on Mechatronics and Automation, ICMA 2006

Volumn 2006, Issue , 2006, Pages 996-1001

  Kinoshita, Takuya ^a   Imado, Fumiaki ^a  

^a SHINSHU UNIVERSITY   (Japan)

Author keywords

Flight simulations; Guidance system; Optimal control; UAV

Indexed keywords

ATTITUDE CONTROL; COMPUTER SIMULATION; OPTIMAL CONTROL SYSTEMS; PARAMETER ESTIMATION; UNMANNED AERIAL VEHICLES (UAV);

FLIGHT MANEUVERS; OPTIMAL FLIGHT CONTROLS;

FLIGHT CONTROL SYSTEMS;

EID: 34247233107     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/ICMA.2006.257761     Document Type: Conference Paper

References (4)

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2. W. P., Gilbert, L. T., Nguyen, and R. W., Van Gunst, "Simulation Study of the Effectiveness of an Automatic Control System Designed to Improve the High-Angle-of-Attack Characteristics of a Fighter Airplane", NASA TND-8176, 1976.
3. A. E, Bryson, Jr., and W. F, Denham, "A Steepest Ascent Method for Solving Optimum Programming Problems", Journal of Applied Mechanics, vol. 29, 1962, pp. 247-257.
4. A. E, Bryson, Jr., and Y. C., Ho, "Applied Optimal Control", Hemisphere Publishing, Washington, D.C., 1975, pp. 221-228.