Optimal decoupling method of attitude control for launch vehicle

Yuhang Xuebao/Journal of Astronautics

Volumn 27, Issue 4, 2006, Pages 783-786

  Li, Lian Zhong ^a   Wang, Xin ^a  

^a Beijing Institute of Control and Electric   (China)

Author keywords

Attitude control; Body coordinate system; Commanded body coordinate system; Decoupling control; Maneuver in changing trajectory

Indexed keywords

COMPUTER SIMULATION; MANEUVERABILITY;

ATTITUDE CONTROL; BODY COORDINATE SYSTEM; COMMANDED BODY COORDINATE SYSTEM; DECOUPLING CONTROL; EULAR ANGLES; LAUNCH VEHICLE; MANEUVER IN CHANGING TRAJECTORY; PITCH CIRCUIT; ROLL CIRCUIT; YAW CIRCUIT;

ROCKETS;

EID: 33751114914     PISSN: 10001328     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (2)

1. CHEN Shi-nian. The Design of Control System[M]. Beijing: The Astrionics Press, 1996
2. JIA Pei-ran, CHEN Ke-jun, HE Li. The Ballistics of Long-Distance Missile[M]. National Univ. of Defense Technology Press, 1993