Proposal of a Unified Control Strategy for Vertical Take-off and Landing Transition Aircraft Configurations
Author:
Affiliation:
1. Technical University of Munich
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3478
Reference19 articles.
1. A simplified approach to nonlinear dynamic inversion based flight control
2. X-35B STOVL Flight Control Law Design and Flying Qualities
3. Robust Flight Control Using Incremental Nonlinear Dynamic Inversion and Angular Acceleration Prediction
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