Automatic Control of VTOL Micro Air Vehicle During Transition Maneuver-Reference-Cited by-同舟云学术

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Automatic Control of VTOL Micro Air Vehicle During Transition Maneuver

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
Short-container-title:

Author:

Chu Diyang¹,Sprinkle Jonathan¹,Randall Ryan¹,Shkarayev Sergey¹

Affiliation:

1. University of Arizona

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-5875

Reference22 articles.

1. Aerodynamic Design of Micro Air Vehicles for Vertical Flight

2. On Fixed-Wing Micro-Air Vehicles with Hovering Capabilities

3. McCormick,B.W.Jr.,AerodynamicsofV/STOLFlight,DoverPublications,Inc.,Mineola,NY,1999.

4. Kohlman,D.,IntroductiontoV/STOLAirplanes,IowaStateUniversityPress,Ames,IA,1981.

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1. An Annular Wing VTOL UAV: Flight Dynamics and Control;Drones;2020-04-26

2. Conceptual design and control of twin-propeller tail-sitter mini-UAV;CEAS Aeronautical Journal;2019-03-12

3. Aerodynamic Modeling and Optimization of a Blended-Wing-Body Transitioning UAV;18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2017-06-02

4. Conceptual Design of a Blended-Wing-Body Tilt-Arm Hybrid Unmanned Aerial Vehicle;58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2017-01-05

5. Longitudinal Aerodynamics of Rapidly Pitching Fixed-Wing Micro Air Vehicles;Journal of Aircraft;2012-03

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