Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque

2014 ◽  
Vol 351 (2) ◽  
pp. 507-524 ◽  
Author(s):  
Ming-Jiang Zhang ◽  
Chang-Yin Zhao
2009 ◽  
Vol 104 (4) ◽  
pp. 337-353 ◽  
Author(s):  
Rodolpho Vilhena de Moraes ◽  
Regina Elaine Santos Cabette ◽  
Maria Cecília Zanardi ◽  
Teresinha J. Stuchi ◽  
Jorge Kennety Formiga

2014 ◽  
Vol 2014 ◽  
pp. 1-15 ◽  
Author(s):  
Chunhui Liang ◽  
Yuanchun Li

Attitude stability analysis and robust control algorithms for spacecrafts orbiting irregular asteroids are investigated in the presence of model uncertainties and external disturbances. Rigid spacecraft nonlinear attitude models are considered and detailed attitude stability analysis of spacecraft subjected to the gravity gradient torque in an irregular central gravity field is included in retrograde orbits and direct orbits using linearized system model. The robust adaptive backstepping sliding mode control laws are designed to make the attitude of the spacecrafts stabilized and responded accurately to the expectation in the presence of disturbances and parametric uncertainties. Numerical simulations are included to illustrate the spacecraft performance obtained using the proposed control laws.


2004 ◽  
Vol 10 (4) ◽  
pp. 39-49
Author(s):  
V.A. Shuvalov ◽  
◽  
G.S. Kochubey ◽  
A.I. Priymak ◽  
N.I. Pismenniy ◽  
...  

Sign in / Sign up

Export Citation Format

Share Document