Rigid body attitude control with inclinometer and low-cost gyro measurements

Systems and Control Letters

Volumn 49, Issue 2, 2003, Pages 151-159

  Akella, Maruthi R ^a   Halbert, James T ^a   Kotamraju, Gnana R ^b  

^a The University of Texas at Austin   (United States)

^b MicroStrategy Inc   (United States)

Author keywords

Attitude control; Inclinometers; Low cost gyros; Modified Rodrigues parameters; Output feedback

Indexed keywords

ASYMPTOTIC STABILITY; CONTROL EQUIPMENT; FEEDBACK CONTROL; KINEMATICS; ROBOT APPLICATIONS; SENSORS; STATE ESTIMATION; VIRTUAL REALITY;

ATTITUDE CONTROL;

NONLINEAR CONTROL SYSTEMS;

EID: 0037881866     PISSN: 01676911     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0167-6911(02)00320-1     Document Type: Article

References (14)

1. Akella M.R. Rigid body attitude tracking without angular velocity feedback. Systems Control Lett. 42(4):2001;321-326.
2. Caccavale F., Villani L. Output feedback control for attitude tracking. Systems Control Lett. 38:1999;91-98.
3. J.L. Junkins, Y. Kim, Introduction to Dynamics and Control of Flexible Structures, AIAA Education Series, Washington, D.C., 1993, pp. 89-91.
4. Junkins J.L., Turner J.D. Optimal Spacecraft Rotational Maneuvers. 1986;Elsevier, Amsterdam, Netherlands.
5. Lizarralde F., Wen J. Attitude control without angular velocity measurement. a passivity approach IEEE Trans. Automat. Control. 41(3):1996;468-472.
6. Marandi S.R., Modi V.J. A preferred coordinate system and the associated orientation representation in attitude dynamics. Acta Astronaut. 15(11):1987;833-843.
7. Rehbinder H., Hu X. Nonlinear state estimation for rigid-body motion with low-pass sensors. Systems Control Lett. 40:2000;183-190.
8. Schaub H., Akella M.R., Junkins J.L. Adaptive control of nonlinear attitude motions realizing linear closed loop dynamics. J. Guidance Control Dynamics. 24(1):2001;95-100.
9. Schaub H., Junkins J.L. Stereographic orientation parameters for attitude dynamics. a generalization of the Rodrigues parameters J. Astronaut. Sci. 44(1):1996;1-19.
10. Schaub H., Robinett R.D., Junkins J.L. Globally stable feedback laws for near-minimum fuel and near-minimum-time pointing maneuvers for a landmark-tracking spacecraft. J. Astronaut. Sci. 44(4):1996;443-466.
11. Shuster M.D. A survey of attitude representations. J. Astronaut. Sci. 41(4):1993;439-517.
12. Tsiotras P. Stabilization and optimality results for the attitude control problem. J. Guidance Control Dynamics. 19(4):1996;772-779.
13. Tsiotras P. Further passivity results for the attitude control problem. IEEE Trans. Automat. Control. 43(11):1998;1597-1600.
14. P. Tsiotras, V. Doumtchenko, Control of Spacecraft Subject to Actuator Failures: State-of-the-art and Open Problems, R.H. Battin Astrodynamics Conference, College Station, TX, AAS 00-264, March, 2000.