Recoverable sets of initial conditions and their use for aircraft flight planning after a loss of control event
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-0786
Reference37 articles.
1. Online Aerodynamic Model Structure Selection and Parameter Estimation for Fault Tolerant Control
2. Flight Control Reconfiguration Based on Online Physical Model Identification and Nonlinear Dynamic Inversion
3. Safe Maneuvering Envelope Estimation based on a Physical Approach
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