Title :
Simulating and analysis for attitude angles of RRP
Author :
Kang, Chunpeng ; Su, Zhong
Author_Institution :
Beijing Inf. Sci. & Technol. Univ., Beijing
Abstract :
The Rotary Rocket Projectile ( RRP) without rudder is mainly studied. First choose the body reference frame as benchmark, Then model to three attitude angle of RRP using Euler method, and employ MATLAB/simulink to simulate them. The results show that when the rotation speed increasing in the appropriate scope can effectively improve the flight stability. However, the pitch angle would produce a certain eccentricity phenomenon.
Keywords :
attitude control; projectiles; rockets; stability; Euler method; attitude angles; flight stability; pitch angle; rotary rocket projectile; rotation speed; Aircraft; Analytical models; Angular velocity; Iron; MATLAB; Mathematical model; Missiles; Projectiles; Rockets; Stability;
Conference_Titel :
System Simulation and Scientific Computing, 2008. ICSC 2008. Asia Simulation Conference - 7th International Conference on
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-1786-5
Electronic_ISBN :
978-1-4244-1787-2
DOI :
10.1109/ASC-ICSC.2008.4675491
