Dynamic Response to Canard Control and Gravity for a Dual-Spin Projectile-Reference-Cited by-同舟云学术

Dynamic Response to Canard Control and Gravity for a Dual-Spin Projectile

Published:2016-05 Issue:3 Volume:53 Page:558-566
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Chang Sijiang¹

Affiliation:

1. Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China

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.A33485

Reference18 articles.

1. Guidance and Control of a Cannon-Launched Guided Projectile

2. Flight Stability of an Asymmetric Projectile with Activating Canards

3. SmithJ. A.SmithK. A.TopliffeR. “Feasibility Study for Application of Modular Guidance and Control Units to Existing ICM Projectiles,” U.S. Army Armament Research and Development Command, Rept. ARLCD-CR-79001, Dover, NJ, Nov. 1978.

Cited by 18 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Nonlinear Model and Ballistic Impact of Body Aerodynamics for Canard Dual-Spin Aircraft;2024

2. Multidisciplinary design optimization of a dual-spin guided vehicle;Defence Technology;2023-11

3. A guidance and control design with reduced information for a dual-spin stabilized projectile;Defence Technology;2023-07

4. Research on Angular Motion Characteristics and Stability of Trajectory-Corrected Rocket Projectile with Isolated Rotating Tail Rudder;Mathematical Problems in Engineering;2023-02-15

5. Investigation of the acceleration influence on friction in bearings in dual-spin missile;Materials Today: Proceedings;2023