Control Inceptor Design for Remote Control of a Transition UAV
Author:
Affiliation:
1. Technical University of Munich
Publisher
American Institute of Aeronautics and Astronautics
Reference15 articles.
1. Proposal of a Unified Control Strategy for Vertical Take-off and Landing Transition Aircraft Configurations
2. Integrated Reference Model for a Tilt-rotor Vertical Take-off and Landing Transition UAV
3. Application of Quantitative Measures for Analysing Aircraft Handling Qualities
4. Real-time Desktop Flying Qualities Evaluation Simulator
5. Influence of Inceptors on Pilot-Aircraft System Characteristics and Flying Qualities
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1. A Linear-Active-Disturbance-Rejection-Based Vertical Takeoff and Acceleration Strategy with Simplified Vehicle Operations for Electric Vertical Takeoff and Landing Vehicles;Mathematics;2022-09-14
2. Increasing Operator Situational Awareness During Transition Procedures for Fixed-Wing VTOL UAV Operations;AIAA Scitech 2021 Forum;2021-01-04
3. Control Inceptor Design for Onboard Piloted Transition VTOL Aircraft Considering Simplified Vehicle Operation;AIAA Scitech 2021 Forum;2021-01-04
4. Defining Robust Transition and Re-Transition Procedures for Unmanned Fixed-Wing VTOL Aircraft;AIAA Scitech 2021 Forum;2021-01-04
5. Thrust command based Integrated Reference Model with Envelope Protections for Tilt-rotor VTOL Transition UAV;AIAA Aviation 2019 Forum;2019-06-14
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