Analysis of Spin-Rate Property for Dual-Spin-Stabilized Projectiles with Canards

Author:

Chang Sijiang1,Wang Zhongyuan1,Liu Tiezheng2

Affiliation:

1. School of Energy and Power Engineering, Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China

2. Department of Military Equipment Trade, Ordnance Science Institute of China, 100089 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Reference13 articles.

1. 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, Picatinny Arsenal, NJ, Nov. 1978.

2. Linear Theory of a Dual-Spin Projectile in Atmospheric Flight

3. BurchettB.PetersonA.CostelloM. “Prediction of Swerving Motion of a Dual-Spin Projectile with Lateral Pulsejets in Atmospheric Flight,” U.S. Army Research Lab., Rept. ARL-CR-570, Aberdeen Proving Ground, MD, Nov. 2005.

4. Course Correction Fuze Concept Analysis for In-Service 155 mm Spin-Stabilized Gunnery Projectiles

5. Wind Tunnel Tests and Open-Loop Trajectory Simulations for a 155 mm Canards Guided Spin Stabilized Projectile

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