Control Allocation Framework for a Tilt-rotor Vertical Take-off and Landing Transition Aircraft Configuration
Author:
Affiliation:
1. Technical University of Munich
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3480
Reference17 articles.
1. Control allocation—A survey
2. Constrained control allocation
3. Constrained control allocation - Three-moment problem
4. Modified Pseudoinverse Redistribution Methods for Redundant Controls Allocation
5. Evaluation of Optimization Methods for Control Allocation
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