Flight Control for a Class of 155 mm Spin-stabilized Projectiles with Course Correction Fuse (CCF)
Author:
Affiliation:
1. French-German Research Institute of Saint-Louis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-6247
Reference20 articles.
1. Survey of gain-scheduling analysis and design
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3. Stability Limits of Spinning Missiles with Attitude Autopilot
4. Attitude Guidance for Spinning Vehicles with Independent Pitch and Yaw Control
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