Spin-axis stabilization of a rigid spacecraft using two reaction wheels

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 5, 2001, Pages 1046-1049

  Kim, S ^a   Kim, Y ^a  

^a Seoul National University   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

ASYMPTOTIC STABILITY; DIFFERENTIAL EQUATIONS; FEEDBACK CONTROL; FLIGHT DYNAMICS; NUMERICAL METHODS; ROTATION; VECTORS;

FEEDBACK CONTROL LAW; INERTIAL AXIS; SPIN AXIS STABILIZATION; TWO REACTION WHEELS;

SPACECRAFT;

EID: 0035441731     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4818     Document Type: Article

References (7)

1. Sliding mode stabilizing control law of under-actuated spacecraft
2. Spin-axis stabilization of symmetric spacecraft with two control torques
3. Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models
4. Attitude stabilization of a rigid spacecraft using two momentum wheel actuators
5. A new parameterization of the attitude kinematics