Dynamic Inversion with Adaptive Augmentation for a High-Speed Guided Projectile
Author:
Affiliation:
1. Texas A&M University
2. Embry-Riddle Aeronautical University
3. Army Research Laboratory Aberdeen Proving Ground
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-2647
Reference22 articles.
1. A Gain-Scheduled Approach for the Control of a High-Speed Guided Projectile
2. Bryson, J., and Gruenwald, B. C. "Automated Gain-Scheduling Approach for Three-Loop Autopilot," Tech. Rep. ARL-TR-9564, DEVCOM Army Research Laboratory, Sep. 2022.
3. Nonlinear Dynamic Inversion Flight Control Design for Guided Projectiles
4. Robust Design for the Roll-Channel Autopilot of a Canard-Guided Dual-Spin Projectile
5. Dynamic Inversion Flight Control Design for Aircraft with Non-Minimum Phase Response
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