Development of air spindle and triaxial air bearing testbeds for spacecraft dynamics and control experiments

Proceedings of the American Control Conference

Volumn 5, Issue , 2001, Pages 3967-3972

  Bernstein, D S ^a   McClamroch, N H ^a   Bloch, A ^a  

^a UNIVERSITY OF MICHIGAN   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL NONLINEARITIES; DEGREES OF FREEDOM (MECHANICS); GRAVITATIONAL EFFECTS; MOTION CONTROL; SPACECRAFT;

AIR SPINDLE; SPACECRAFT CONTROL; SPACECRAFT DYNAMICS; TRIAXIAL AIR BEARING;

CONTROL SYSTEM SYNTHESIS;

EID: 0034848833     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2001.946287     Document Type: Conference Paper

References (16)

1. Naive control of the double integrator: A comparison of a dozen diverse controllers under off-nominal conditions
2. Asymptotic tracking of spacecraft attitude motion with inertia identification
3. Nonlinear feedback control with global stabilization
4. Rotational stabilization of a rigid body using two torque actuators
5. Attitude stabilization of a rigid spacecraft using two control torques: A nonlinear control approach based on the spacecraft attitude dynamics
6. Attitude stabilization of a rigid spacecraft using two momentum wheel actuators
7. Stabilization of rigid body dynamics by internal and external torques
8. Controlled lagrangians and the stabilization of Euler-Poincaré mechanical systems
9. Three dimensional attitude and shape control of spacecraft with appendages and reaction wheels
10. Nonlinear attitude and shape control of spacecraft with appendages and reaction wheels
11. Dynamics and control of a class of underactuated mechanical systems
12. Discontinuous feedback control of a special class of underactuated mechanical systems
13. Feedback control of a space vehicle with unactuated fuel slosh dynamics