Author: Tarek M. M. Abdel-RahmanPublisher: Toronto, Ont., University of Toronto
ISBN:
Category : Space vehicles
Languages : en
Pages : 272
Book Description
The Effects of Structural Flexibility on the Nonlinear Attitude Control of Spacecraft
Author: Tarek M. M. Abdel-RahmanPublisher: Toronto, Ont., University of Toronto
ISBN:
Category : Space vehicles
Languages : en
Pages : 272
Book Description
Effects of Structural Flexibility on Spacecraft Control Systems
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 52
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Technology for Large Space Systems
Author: Publisher:
ISBN:
Category : Large space structures (Astronautics)
Languages : en
Pages : 172
Book Description
UTIAS Report
Author: University of Toronto. Institute for Aerospace StudiesPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 680
Book Description
Effects of Structural Flexibility on Launch Vehicle Control Systems
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 60
Book Description
Effects of Structural Flexibility on Spacecraft Control Systems
Author: National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Technical Abstract Bulletin
Author: Space Station Systems
Author: Control of Nonlinear Multibody Flexible Space Structures
Author: Atul G. KelkarPublisher: Springer
ISBN: 9783662196410
Category : Technology & Engineering
Languages : en
Pages : 144
Book Description
Addressing the difficult problem of controlling flexible spacecraft having multiple articulated appendages is the aim of this volume. Such systems are needed for space mission concepts including multi-payload space platforms and autonomous space-based manipulators. These systems are characterised by highly nonlinear dynamics, flexibility in members and joints, low inherent damping, and modeling uncertainty. A complete nonlinear rotational dynamic model of a generic multibody flexible system is derived, and is shown to possess certain passivity properties. The main result is a class of passivity-based nonlinear and linear output feedback control laws that enable globally stable closed-loop manoeuvres. The control laws are robust to parametric uncertainties, unmodeled uncertainties, and in some cases, actuator and sensor nonlinearities. All results given are also applicable to flexible terrestrial manipulators.