Output Tracking of Non-Minimum Phase Dynamics
Author:
Affiliation:
1. Texas A&M University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6487
Reference22 articles.
1. Autopilot design for highly maneuvering STT missiles via singular perturbation-like technique
2. Nonlinear control design for slightly non-minimum phase systems: Application to V/STOL aircraft
3. Approximate output tracking for nonlinear non-minimum phase systems with an application to flight control
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3. Feedback Control of a Nonlinear Non-Minimum Phase Missile with Limited Modeling Information;AIAA Guidance, Navigation, and Control Conference;2015-01-02
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