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Effects Of Structural Flexibility On Spacecraft Control Systems
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Book Synopsis Effects of Structural Flexibility on Spacecraft Control Systems by : United States. National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Spacecraft Control Systems written by United States. National Aeronautics and Space Administration and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Structural Flexibility on Spacecraft Control Systems by : National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Spacecraft Control Systems written by National Aeronautics and Space Administration and published by . This book was released on 1969 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Structural Flexibility on Launch Vehicle Control Systems by : United States. National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Launch Vehicle Control Systems written by United States. National Aeronautics and Space Administration and published by . This book was released on 1970 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Structural Flexibility on Entry Vehicle Control Systems by : United States. National Aeronautics and Space Administration
Download or read book Effects of Structural Flexibility on Entry Vehicle Control Systems written by United States. National Aeronautics and Space Administration and published by . This book was released on 1972 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Survey of Structural Flexibility Effects on Spacecraft Control Systems by : Richard B. Noll
Download or read book A Survey of Structural Flexibility Effects on Spacecraft Control Systems written by Richard B. Noll and published by . This book was released on 1969 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Structural Flexibility on Launch Vehicle Control Systems by : R. B. Noll
Download or read book Effects of Structural Flexibility on Launch Vehicle Control Systems written by R. B. Noll and published by . This book was released on 1970 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Space Vehicle Design Criteria (Guidance and Control) Publisher : ISBN 13 : Total Pages :62 pages Book Rating :4.:/5 (111 download)
Book Synopsis Effects of Structural Flexibility on Entry Vehicle Control Systems by : United States. National Aeronautics and Space Administration. Space Vehicle Design Criteria (Guidance and Control)
Download or read book Effects of Structural Flexibility on Entry Vehicle Control Systems written by United States. National Aeronautics and Space Administration. Space Vehicle Design Criteria (Guidance and Control) and published by . This book was released on 1972 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effects of Structural Flexibility on the Nonlinear Attitude Control of Spacecraft by : Tarek M. M. Abdel-Rahman
Download or read book The Effects of Structural Flexibility on the Nonlinear Attitude Control of Spacecraft written by Tarek M. M. Abdel-Rahman and published by Toronto, Ont., University of Toronto. This book was released on 1977 with total page 272 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flexible Spacecraft Dynamics, Control and Guidance by : Leonardo Mazzini
Download or read book Flexible Spacecraft Dynamics, Control and Guidance written by Leonardo Mazzini and published by Springer. This book was released on 2015-10-27 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is an up-to-date compendium on spacecraft attitude and orbit control (AOC) that offers a systematic and complete treatment of the subject with the aim of imparting the theoretical and practical knowledge that is required by designers, engineers, and researchers. After an introduction on the kinematics of the flexible and agile space vehicles, the modern architecture and functions of an AOC system are described and the main AOC modes reviewed with possible design solutions and examples. The dynamics of the flexible body in space are then considered using an original Lagrangian approach suitable for the control applications of large space flexible structures. Subsequent chapters address optimal control theory, attitude control methods, and orbit control applications, including the optimal orbital transfer with finite and infinite thrust. The theory is integrated with a description of current propulsion systems, with the focus especially on the new electric propulsion systems and state of the art sensors and actuators.
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781722978686 Total Pages :132 pages Book Rating :4.9/5 (786 download)
Book Synopsis Control-Structure Interaction/Mirror Motion Compensation by : National Aeronautics and Space Administration (NASA)
Download or read book Control-Structure Interaction/Mirror Motion Compensation written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: Space Systems/Loral (formerly Ford Aerospace, Space Systems Division) has implemented a rigid-body Mirror Motion Compensation (MMC) scheme for the GOES-I/M spacecraft currently being built for NASA and NOAA. This has resulted in a factor of 15 reduction in pointing error due to rigid-body spacecraft motion induced by the periodic black-body calibration maneuvers required for the instruments. For GOES the spacecraft and the payload mirrors are considered as rigid bodies. The structural flexibility effects are small and are included in the total pointing budget as a separate item. This paper extends the MMC technique to include structural flexibility. For large multi-payload platforms, the structural flexibility effects can be more important in sensor pointing jitter as the result of payload motion. Sensitivity results are included to show the importance of the dynamic model fidelity. Mclaren, Mark and Chu, Peter and Price, Xen Unspecified Center CONTROL SYSTEMS DESIGN; GOES SATELLITES; INSTRUMENT COMPENSATION; MIRRORS; POINTING CONTROL SYSTEMS; SATELLITE-BORNE INSTRUMENTS; SPACECRAFT INSTRUMENTS; DYNAMIC CONTROL; FEEDBACK CONTROL; INSTRUMENT ERRORS; POSITION ERRORS; SENSITIVITY; SPACECRAFT MOTION; VIBRATION DAMPING...
Book Synopsis Structural Dynamics and Control Interaction of Flexible Structures by : Robert Samuel Ryan
Download or read book Structural Dynamics and Control Interaction of Flexible Structures written by Robert Samuel Ryan and published by . This book was released on 1987 with total page 752 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Effects of Extreme Structural Flexibility on Flight Vehicles with Feeback-control-system Stabilization by : H.I. Flomenhoft
Download or read book Investigation of Effects of Extreme Structural Flexibility on Flight Vehicles with Feeback-control-system Stabilization written by H.I. Flomenhoft and published by . This book was released on 1965 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781724739353 Total Pages :28 pages Book Rating :4.7/5 (393 download)
Book Synopsis The Dynamics and Control of Large Flexible Space Structures by : National Aeronautics and Space Administration (NASA)
Download or read book The Dynamics and Control of Large Flexible Space Structures written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-08-06 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The dynamics and attitude and shape control of very large, inherently flexible spacecraft systems were investigated. Increasingly more complex examples were examined, beginning with a uniform free-free beam, next a free-free uniform plate/platform and finally by considering a thin shallow spherical shell structure in orbit. The effects devices were modeled. For given sets of assumed actuator locations, the controllability of these systems was first established. Control laws for each of the actuators were developed based on decoupling techniques (including distributed modal control) pole placement algorithms and a application of the linear regulator problem for optical control theory. Bainum, P. M. and Krishna, R. and Kumar, V. K. and Reddy, A. S. S. R. Unspecified Center NASA-CR-164982 NSG-1414
Book Synopsis Technology for Large Space Systems by :
Download or read book Technology for Large Space Systems written by and published by . This book was released on 1982 with total page 460 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Space Station Systems written by and published by . This book was released on 1987 with total page 252 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters by : Jie Wang
Download or read book Rigid-Flexible Coupling Dynamics and Control of Flexible Spacecraft with Time-Varying Parameters written by Jie Wang and published by Springer Nature. This book was released on 2021-09-15 with total page 190 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book presents the dynamic modeling and attitude control of flexible spacecraft with time-varying parameters. The dynamic characteristics, vibration control methods and attitude stabilization methods for spacecraft are systematically studied in respects of the theoretical modeling, numerical simulation and the ground experiment. Three active control theories in complex mode space are presented for flexible space structures. Optimal slew strategies based on variable amplitudes input shaping methods and coupling control methods are proposed for stabilization of flexible spacecraft. The research provides an important way to solve the problem of high-precision attitude control of flexible spacecraft with time-varying parameters. This book is appropriate for the researchers who focus on the multi-body dynamics, attitude and vibration control of flexible spacecraft.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1985 with total page 828 pages. Available in PDF, EPUB and Kindle. Book excerpt:
