Global stabilization of flexible multibody spacecraft using quaternion-based nonlinear control law

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 5, 1996, Pages 1186-1188

  Kelkar, A G ^a,c   Joshi, S M ^b,d  

^a KANSAS STATE UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Mechanical Engineering Department   (United States)

^d Flight Dynamics and Control Division   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ASYMPTOTIC STABILITY; COMPUTER SIMULATION; DAMPING; DEGREES OF FREEDOM (MECHANICS); EIGENVALUES AND EIGENFUNCTIONS; EQUATIONS OF MOTION; ERROR ANALYSIS; FLEXIBLE STRUCTURES; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; PARAMETER ESTIMATION; SPACECRAFT;

FLEXIBLE MULTIBODY SPACECRAFT; LARGE ANGLE MANEUVERS; PARAMETRIC UNCERTAINTY; QUATERNION-BASED NONLINEAR CONTROL LAW; SCALAR GAIN CONTROL LAW;

CONTROL THEORY;

EID: 0030241258     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.21764     Document Type: Note

References (4)

1. Kelkar, A. G., Joshi, S. ML, and Alberts, T. E., "Dissipative Controllers for Nonlinear Multibody Flexible Space Systems," Journal of Guidance, Control and Dynamics, Vol. 18, No. 5, 1995, pp. 1044-1052.
2. Joshi, S. M., Kelkar, A. G, and Wen, J. T.-Y., "Robust Attitude Stabilization of Spacecraft Using Nonlinear Quaternion Feedback," IEEE Transactions on Automatic Control, Vol. 40, No. 10, 1995, pp. 1800-1803.
3. Kelkar, A. G., "Mathematical Modeling of a Class of Multibody Flexible Space Structures," NASA TM-109166, Dec. 1994.
4. Haug, E. J., Computer-Aided Kinematics and Dynamics of Mechanical Systems, Allyn and Bacon Series in Engineering, Allyn and Bacon, Boston, 1989.