TAILIEUCHUNG - Command shaped robust control of a flexible spacecraft

In this paper a model of a hypothetical flexible spacecraft that resembles French multi mission satellite SPOT is selected. This model represents a multivariable system that is difficult to control due to strong cross couplings. | Journal of Automation and Control Engineering Vol. 6, No. 1, June 2018 Command Shaped Robust Control of a Flexible Spacecraft Waseem A. Butt Department of Electrical Engineering, College of Electrical and Mechanical Engineering, Rawalpindi, Pakistan Email: butt_waseem@ for flexible space structures must meet tight performance requirements while being robust to model uncertainties. Conventional control methods have been used very effectively to control a wide variety of systems. These methods are time tested and are presently being used in most of the industries. In order to carry out analysis of multivariable systems that are coupled, conventional control methods are not so easily manageable. Extensive research has been focused on control of flexible multivariable systems. Attitude control of satellites has been tackled by the help of Self Organizing Fuzzy Logic Controllers (FLC), being a suitable candidate, as engineering experience is usually not available for a satellite system for matching performance through fixed fuzzy rules. Such type of controllers are thus more robust than the fixed rule controllers but the outcome is not always optimum [3], [4]. An integrated feedback/feedforward control system is proposed by [5], for reducing the vibration of flexible structures for large-angle attitude manoeuvre of the spacecraft. Lyapunov based control integrated with the Nil-Mode-Exciting profiler and an extended Input Shaping technique is utilized to effectively improve the transient vibration of the modal response. Vibration suppression is a desirable feature; active vibration suppression for a two-link flexible manipulator is proposed by [6]. This scheme is composed of an input shaper assisted by piezo actuator for active suppression of residual vibrations. This scheme is, however not suitable for a satellite system in which installation of piezo actuators is not practically viable. Design method that is more systematic is always preferable, as by .

• Cơ khí - Chế tạo máy
• Journal of Automation and Control Engineering
• Command shaped robust control of a flexible spacecraft
• Command shaped robust control
• Strong cross couplings
• Loop shaping design
• Increasing the productivity of automation tool by developing socket
• Automation tool by developing socket
• Auto report generated
• The automation tool
• Abnormality management in industrial automation systems
• Industrial automation systems
• Future industrial automation systems
• Abnormality management approach
• Sliding mode based relative pose synchronous control
• Space autonomous rendezvous
• Relative pose synchronous control
• The control system design
• The sliding mode control law
• Application of pressure control type quasiservo valve
• Force control system
• The quasi servo valve
• The pneumatic cylinder
• Robust vehicle suspension system
• Converting active & passive control
• A vehicle to semi active control system analytically
• Semi Active Vehicle System
• Environmental control of a greenhouse system
• NI embedded systems technology
• The soil moisture
• The Engineering School of Bahrain Polytechnic
• Design of control system for 3D printer
• DSP and FPGA
• Control system for 3D printer
• Closed loop control
• Improving performances of a cement rotary kiln
• A model predictive control solution
• Cement rotary kiln
• Advanced process control
• Model predictive control
• Active learning in motor control and matlab simulation
• Active learning in motor control
• Servo motors of the simulation of neural networks
• Motion of a robot arm
• Redundancy and operation of power control system
• A deep space small probe
• Functions of redundancy
• Power Control Unit
• Closed loop speed control of miniature brushless DC motors
• Closed loop speed control
• Miniature brushless DC motors
• Delta Connected BLDC motors
• Adaptive wavelet backstepping control
• Class of mimo underactuated systems
• Multi input multi output
• Proposed control scheme
• Adaptive backstepping controller
• Hybrid position force control for a stewart platform
• Hybrid position force control
• The work surface
• The stewart platform
• Robust control of double inverted pendulum system
• Double inverted pendulum system
• Reference trajectory control
• The dynamic modeling
• Speech recognition in human computer interactive control
• Computer interactive control
• HTK and Sphinx
• Vietnamese speech recognition
• Human computer interaction
• Optimal control of vehicle active suspension system
• Vehicle active suspension system
• The active suspension system
• LQR control technique
• Mimo fuzzy control for autonomous mobile robot
• Mimo fuzzy control
• Autonomous mobile robot
• Implementation of multi input multi output
• Reach defined target
• Asynthesis method of robust cascade control system
• Robust cascade control system
• Imposes robust conditions
• Soft oscillation index
• Efficient adaptive fuzzy control scheme for industrial manipulators
• Degree of freedom
• Fuzzy control scheme
• IMO nonlinear second order systems
• Multilevel inverter topology and control techniques
• Reduce electromagnetic interference
• Control strategies employed
• Linear quadratic optimal control problem of stochastic switching systems
• Linear quadratic optimal control problem
• Stochastic switching systems
• Non invariant linear systems
• Investigation of hybrid adaptive control schemes
• Needle free jet injection system
• Hybrid adaptive control schemes
• Needle free jet injection
• Modelling and simulations
• Development of a new algorithm
• Control excitation of particular mode of a building
• Particular mode of a building
• Sliding mode control
• Control of electric motor machine tools
• Self organizing fuzzy logic controller
• Modify the control rule
• The self organizing fuzzy logic controller