Swerve Solution for Spin-Stabilized Projectiles with Canards: A Revisit
Author:
Affiliation:
1. Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China
2. Science and Technology on Transient Impact Laboratory, 102202 Beijing, People’s Republic of China
Funder
Fundamental Research Funds for the Central Universities
Foundation of Science and Technology on Transient Impact Laboratory
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34964
Reference20 articles.
1. Linear Theory of a Dual-Spin Projectile in Atmospheric Flight
2. Modelling and Stability Analysis for a Class of 155 mm Spin-stabilized Projectiles with Course Correction Fuse (CCF)
3. Guidance and Control Design for a Class of Spin-Stabilized Fin-Controlled Projectiles
4. Flight stability of a dual-spin projectile with canards
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2. Guidance and Control of Spin-Stabilized Projectiles Based on Super Twisting Algorithm;Journal of Guidance, Control, and Dynamics;2023-03
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