NDLI: RBFNN-Based Sliding Mode Control for Flexible Spacecraft Vibration Suppress

Content Provider	IEEE Xplore Digital Library
Author	Qiang Tang Yan Wang Yongjun Lei Xinglin Chen
Copyright Year	2009
Abstract	Vibration suppress of a flexible spacecraft during attitude maneuvering is a challenging task. In this paper, the proposed control includes two major parts: command profile is designed to maneuver a flexible spacecraft with very little residual vibration and an intelligent control scheme consists of an online radial basis function neural network(RBFNN) based slide mode control is performed such that improved tracking accuracy is accomplished in the presence of parametric uncertainties. The input shape is designed to modify the command for elimination of the residual vibration in the open loop, and an RBF neural network based slide mode control law is proposed to achieve system stability and good performance in the closed-loop. With the proposed control law, simulation results verified that the control scheme can achieve the maneuver with high accuracy of little residual vibration.
Starting Page	194
Ending Page	197
File Size	292294
Page Count	4
File Format	PDF
ISBN	9780769538594
DOI	10.1109/IITA.2009.321
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2009-11-21
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Uncertainty input shape Stability slide mode Open loop systems Control systems Sliding mode control Space vehicles Shape control RBFNN Neural networks flexible spacecraft Vibration control Intelligent control
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

A self-adjusting sliding-mode control based on RBF neural network for flexible spacecraft attitude

Sliding mode and shaped input vibration control of flexible systems

Control Input Saturation Sliding-Mode Control System Design for Spacecraft Based on Neural Network

A Combined Positive Position Feedback and Variable Structure Approach for Flexible Spacecraft under Input Nonlinearity

Attitude and Vibration Control in Nonlinear Flexible Spacecraft via Trajectory Shaping and Adaptive Sliding Control

Sliding Mode Attitude and Vibration Control of Flexible Spacecraft with Actuator Dynamics

Vibration suppression and sliding mode attitude control of flexible spacecraft with unknown disturbance and uncertainty

Vibration suppress of flexible spacecraft considering the effects of gravity

Sliding Mode Control Design for Nonlinear Systems Without Reaching Phase and its Applications to a Flexible Spacecraft

RBFNN-Based Sliding Mode Control for Flexible Spacecraft Vibration Suppress

Similar Documents

A self-adjusting sliding-mode control based on RBF neural network for flexible spacecraft attitude

Sliding mode and shaped input vibration control of flexible systems

Control Input Saturation Sliding-Mode Control System Design for Spacecraft Based on Neural Network

A Combined Positive Position Feedback and Variable Structure Approach for Flexible Spacecraft under Input Nonlinearity

Attitude and Vibration Control in Nonlinear Flexible Spacecraft via Trajectory Shaping and Adaptive Sliding Control

Sliding Mode Attitude and Vibration Control of Flexible Spacecraft with Actuator Dynamics

Vibration suppression and sliding mode attitude control of flexible spacecraft with unknown disturbance and uncertainty

Vibration suppress of flexible spacecraft considering the effects of gravity

Sliding Mode Control Design for Nonlinear Systems Without Reaching Phase and its Applications to a Flexible Spacecraft

RBFNN-Based Sliding Mode Control for Flexible Spacecraft Vibration Suppress