DocumentCode
3391859
Title
Simulating and analysis for attitude angles of RRP
Author
Kang, Chunpeng ; Su, Zhong
Author_Institution
Beijing Inf. Sci. & Technol. Univ., Beijing
fYear
2008
fDate
10-12 Oct. 2008
Firstpage
903
Lastpage
905
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;
fLanguage
English
Publisher
ieee
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
Type
conf
DOI
10.1109/ASC-ICSC.2008.4675491
Filename
4675491
Link To Document