Reentry Flight Controller Design Using Nonlinear Dynamic Inversion
Author:
Affiliation:
1. Delft University of Technology, 2600 GB Delft, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/2.3916
Reference28 articles.
1. Entry Trajectory Tracking Law via Feedback Linearization
2. Adaptive on-board guidance for entry vehicles
3. Worst-Case Analysis of the X-38 Crew Return Vehicle Flight Control System
4. Slotine, J., and Li, W., Applied NonlinearControl, 1st ed.Prentice-Hall, Upper SaddleRiver, NJ,1987, pp.207-271.
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