Stability Analysis for Incremental Nonlinear Dynamic Inversion Control
Author:
Affiliation:
1. Delft University of Technology, 2629 HS Delft, The Netherlands
2. Hong Kong Polytechnic University, Hung Hom, Hong Kong, People’s Republic of China
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
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G003791
Reference30 articles.
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2. Flight control design using robust dynamic inversion and time-scale separation
3. Robust Nonlinear Dynamic Inversion Control for a Hypersonic Cruise Vehicle
4. Stability Metrics for Simulation and Flight-Software Assessment and Monitoring of Adaptive Control Assist Compensators
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