Books on the topic 'Flexible Spacecraft Control'

Suhada, Jayasuriya, Texas A & M University., and Lyndon B. Johnson Space Center., eds. Active vibration control techniques for flexible space structures. Texas A&M University, 1990.

Wang, Jie, and Dong-Xu Li. Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-5097-0.

Chun, Hon M. Large-angle slewing maneuvers for flexible spacecraft. Langley Research Center, 1988.

Taylor, Lawrence W. 4th NASA Workshop on Computational Control of Flexible Aerospace Systems: Proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at the Kingsmill Resort, Williamsburg, Virginia, July 11, 1990. Langley Reseearch Center, 1991.

Hailey, Jeffrey A. Experimental verification attitude control techniques for flexible spacecraft slew maneuvers. Naval Postgraduate School, 1992.

McLaren, David Stuart. The use of observers in the control of large, flexible spacecraft. Dept. of Aerospace Science and Engineering, 1985.

Cameron, Ian. Operating the Daisy facility to perform control experiments. University of Toronto, Graduate Dept. of Aerospace Science and Engineering, 1993.

MacMartin, D. G. Frequency shaped cost functionals in the design of control systems for large flexible space structures. Division of Engineering Science, Faculty of Applied Science and Engineering, University of Toronto, 1987.

United States. National Aeronautics and Space Administration., ed. Fuzzy based attitude controller for flexible spacecraft with on/off thrusters. National Aeronautics and Space Administration, 1993.

F, Masri S., Miller R. K, and United States. National Aeronautics and Space Administration, eds. Evaluation of on-line pulse control for vibration suppression in flexible spacecraft. National Aeronautics and Space Administration, 1987.

F, Masri S., Miller R. K, and United States. National Aeronautics and Space Administration, eds. Evaluation of on-line pulse control for vibration suppression in flexible spacecraft. National Aeronautics and Space Administration, 1987.

Taylor, Larry. Workshop on Computational Aspects in the Control of Flexible Systems, held at the Royce Hotel in Williamsburg, Va., July 12-14, 1988: Proceedings. Langley Research Center, 1988.

Ryan, Robert S. Structures dynamics and control interaction of flexible structures: Proceedings of a workshop held at George C. Marshall Space Flight Center, Huntsville, Ala., Apr. 22-24, 1986. Marshall Space Flight Center, 1987.

P. Th. L. M. van Woerkom. Dynamics of flexible spacecraft: An analysis of approaches toward mathematical model order reduction. National Aerospace Laboratory, 1985.

P. Th. L. M. van Woerkom. Dynamics of flexible spacecraft: The internal balancing approach towards mathematical model order reduction. National Aerospace Laboratory, 1985.

Carroll, Kieran Anthony. A balanced subsystem order reduction method. University of Toronto, Graduate Dept. of Aerospace Science and Engineering, 1993.

Wright, Robert L. NASA/DOD control structures interaction technology 1986: Proceedings of a conference sponsored by NASA Langley Research Center, Hampton, Virginia, and Air Force Wright Aeronautical Laboratories, Wright-Patterson, AFB, Ohio, and held in Norfolk, Virginia, November 18-21, 1986. Langley Research Center, 1986.

Akoh-Arrey, Ayuk A. A comparison of sliding mode control systems for flexible spacecraft with unknown dynamics. UEL, 1993.

Dietz, Peter Robert Wilhelm. Determination of the efficacy of using accelerometers as sensors for third generation satellites. Institute for Aerospace Studies, 1986.

Dietz, Peter Robert Wilhelm. Determination of the efficacy of using accelerometers as sensors for third generation satellites. Dept. of Aerospace Science and Engineering, University of Toronto, 1986.

Joshi, S. M. A class of stabilizing controllers for flexible multibody systems. National Aeronautics and Space Administration, Langley Research Center, 1995.

1934-, Craig Roy R., and Lyndon B. Johnson Space Center., eds. A decentralized linear quadratic control design method for flexible structures: Interim report. Center for Aeromechanics Research, University of Texas at Austin, 1990.

Crocker, G. W. Digital real-time control of Daisy's reaction wheels, ribs and hub. Dept. of Aerospace Science and Engineering, 1989.

United States. National Aeronautics and Space Administration., ed. Final technical report on robust design of distributed controllers for large flexible space structures. Catholic University of America, School of Engineering and Architecture, Dept. of Electrical Engineering, 1988.

United States. National Aeronautics and Space Administration., ed. Dynamics and control of flexible spacecraft during and after slewing maneuvers: NASA grantee annual report. National Aeronautics and Space Administration, 1990.

Jones, Evan S. Development of an active damping system to aid in the attitude control of flexible spacecraft. Naval Postgraduate School, 1991.

Larry, Taylor, and Langley Research Center, eds. 4th Annual NASA SCOLE Workshop. National Aeronautics and Space Administration, Langley Research Center, 1988.

L, Wright Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. NASA/DOD control/structures interaction technology, 1986: Proceedings of a conference ... held in Norfolk, Virginia, November 18-21, 1986. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

L, Wright Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. NASA/DOD control/structures interaction technology, 1986: Proceedings of a conference ... held in Norfolk, Virginia, November 18-21, 1986. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Ronnie, Francis, Wells Eugene M, bd Systems Inc, and United States. National Aeronautics and Space Administration., eds. Final report for research study entitled "Performance evaluation of the Gravity Probe B design": Contract number NAS8-40618. National Aeronautics and Space Administration, 1996.

Ronnie, Francis, Wells Eugene M, bd Systems Inc, and United States. National Aeronautics and Space Administration., eds. Final report for research study entitled "Performance evaluation of the Gravity Probe B design": Contract number NAS8-40618. National Aeronautics and Space Administration, 1996.

Center, Langley Research, ed. Experimental validation of an integrated controls-structures design methodology for a class of flexible space structures. National Aeronautics and Space Administration, Langley Research Center, 1994.

Phan, Minh Q. Stochastic prediction of vibration levels in the presence of modeling uncertainties: Final report, NASA grant NAG1-1698. Princeton University, Dept. of Mechanical and Aerospace Engineering, 1997.

Revi, Sinha, and United States. National Aeronautics and Space Administration., eds. Robust on-off pulse control of flexible space vehicles: Final report of the second-year project. Research Institute for COmputing and Information Systems, University of Houston-Clear Lake, 1993.

Revi, Sinha, and United States. National Aeronautics and Space Administration., eds. Robust on-off pulse control of flexible space vehicles: Final report of the second-year project. Research Institute for COmputing and Information Systems, University of Houston-Clear Lake, 1993.

Revi, Sinha, and United States. National Aeronautics and Space Administration., eds. Robust on-off pulse control of flexible space vehicles: Final report of the second-year project. Research Institute for COmputing and Information Systems, University of Houston-Clear Lake, 1993.

Meirovitch, Leonard. A progress report on identification and control of structures in space: NASA research grant NAG-1-225, covering the period July 1 - June 31, 1985. Virginia Pollytechnic Institute and State University , Engineering Science and Mechanics Dept., 1985.

Meirovitch, Leonard. A progress report on identification and control of structures in space: NASA research grant NAG-1-225, covering the period January 1 - June 30, 1985. National Aeronautics and Space Administration?], 1985.

United States. National Aeronautics and Space Administration., ed. Evaluation of a pulse control law for flexible spacecraft: Final technical report : reporting period 1 June 1984 - 31 May 1985. National Aeronautics and Space Administration, 1985.

United States. National Aeronautics and Space Administration, ed. Evaluation of a pulse control law for flexible spacecraft: Final technical report : reporting period 1 June 1984 - 31 May 1985. National Aeronautics and Space Administration, 1985.

A, King James, Phillips Douglas J, and Langley Research Center, eds. Streamlined design and self reliant hardware for active control of precision space structures. National Aeronautics and Space Administration, Langley Research Center, 1994.

NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems (1992 Williamsburg, Va.). NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems: Proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington, D.C. and held in Williamsburg, Virginia, June 8-10, 1992. National Aeronautics and Space Administration, Langley Research Center, 1994.

B, Marks Virginia, Keckler Claude R, and Langley Research Center, eds. NASA Workshop on Distributed Parameter Modeling and Control of Flexible Aerospace Systems: Proceedings of a workshop sponsored by tne National Aeronautics and Space Administration, Washington, D.C. and held in Williamsburg, Virginia, June 8-10, 1992. National Aeronautics and Space Administration, Langley Research Center, 1994.

Maghami, Peiman G. An optimization-based integrated controls-structures design methodology for flexible space structures. Langley Research Center, 1993.