Incremental Control and Guidance of Hybrid Aircraft Applied to a Tailsitter Unmanned Air Vehicle
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
2. ENAC, F-31055 Toulouse, France
Funder
Delphi Consortium
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Reference16 articles.
1. Unified Velocity Control and Flight State Transition of Unmanned Tilt-Wing Aircraft
2. Simulator Development for Transition Flight Dynamics of a VTOL MAV
3. Flight-Test Results of Autonomous Airplane Transitions Between Steady-Level and Hovering Flight
4. Flight Testing of the T-Wing Tail-Sitter Unmanned Air Vehicle
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