Intelligent Control Management of Autonomous Air Vehicles

2006 ◽  
Author(s):  
Mario Innocenti ◽  
Lorenzo Pollini ◽  
Andrea Bracci
Keyword(s):  
Intelligent Control ◽  
Autonomous Air Vehicles ◽  
Control Management ◽  
Air Vehicles

Departure resilient control for autonomous air vehicles

2009 ◽  
Author(s):  
James A. Ramsey ◽  
Ryan T. Ratliff ◽  
Kevin A. Wise ◽  
Eugene Lavretsky
Keyword(s):  
Resilient Control ◽  
Autonomous Air Vehicles ◽  
Air Vehicles

An insect-inspired targeting/evasion reflex for autonomous air vehicles

2003 ◽  
Author(s):  
R. Vaidyanathan ◽  
C.A. Williams ◽  
T.S. Prince ◽  
R.E. Ritzmann ◽  
R.D. Quinn
Keyword(s):  
Autonomous Air Vehicles ◽  
Air Vehicles

scholarly journals Dynamic analysis and qft-based robust control design of a coaxial micro-helicopter

2019 ◽  
Vol 9 (5) ◽  
pp. 4099
Author(s):  
Meksi Aissa ◽  
Ahmed Hamida Boudinar ◽  
Benatman Kouadri
Keyword(s):  
Design Method ◽  
Control Law ◽  
Quantitative Feedback Theory ◽  
Uncertain Disturbances ◽  
Performance Specifications ◽  
Autonomous Air Vehicles ◽  
Robust Control Design ◽  
Poles And Zeros ◽  
Micro Helicopter ◽  
Air Vehicles

This paper presents the dynamic behavior of a coaxial micro-helicopter, under Quantitative Feedback Theory (QFT) control. The flight dynamics of autonomous air vehicles (AAVs) with rotating rings is non-linear and complex. Then, it becomes necessary to characterize these non-linearities for each flight configuration, in order to provide these autonomous air vehicles (AAVs) with autonomous flight and navigation capabilities. Then, the nonlinear model is linearized around the operating point using some assumptions. Finally, a robust QFT control law over the coaxial micro-helicopter is applied to meet some specifications. QFT (quantitative feedback theory) is a control law design method that uses frequency domain concepts to meet performance specifications while managing uncertainty. This method is based on the feedback control when the plant is uncertain or when uncertain disturbances are affecting the plant. The QFT design approach involves conventional frequency response loop shaping by manipulating the gain variable with the poles and zeros of the nominal transfer function. The design process is accomplished by using MATLAB environment software.

Near-Optimal Horizontal Trajectories for Autonomous Air Vehicles

1997 ◽  
Vol 20 (4) ◽  
pp. 735-741 ◽  
Author(s):  
Ilana Shapira ◽  
Joseph Z. Ben-Asher
Keyword(s):  
Autonomous Air Vehicles ◽  
Air Vehicles
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