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  1. Journal of Computer and Systems Sciences International
  2. Journal of Computer and Systems Sciences International : Volume 54
  3. Journal of Computer and Systems Sciences International : Volume 54, Issue 1, January 2015
  4. Kinematically optimal spacecraft attitude control
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Journal of Computer and Systems Sciences International : Volume 56
Journal of Computer and Systems Sciences International : Volume 55
Journal of Computer and Systems Sciences International : Volume 54
Journal of Computer and Systems Sciences International : Volume 54, Issue 6, November 2015
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Journal of Computer and Systems Sciences International : Volume 54, Issue 3, May 2015
Journal of Computer and Systems Sciences International : Volume 54, Issue 2, March 2015
Journal of Computer and Systems Sciences International : Volume 54, Issue 1, January 2015
Interval stability of linear impulsive systems
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Conditions of anisotropic norm boundedness for descriptor systems
Qualitative analysis of optimal trajectories of the point mass motion in a resisting medium and the brachistochrone problem
Control of resource-intensive computations under uncertainty. III. Dynamic concurrent resource allocation
Resource allocation algorithm in data centers with a unified scheduler for different types of resources
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Investigation of the polyharmonic method for calculating frequency responses of nonlinear dynamic plants
Nonlinear integer transportation problem with additional supply and consumption points
Stabilization of coupled motions of an aircraft in the pitch-yaw channels in the absence of information about the sliding angle: Analytical synthesis
A solution of the navigation problem for autonomous insertion of payload into a geostationary orbit using a low-thrust engine
Kinematically optimal spacecraft attitude control
A new atmospheric GNSS method for improving the absolute positioning accuracy
Physical characteristics of the sensing elements of feedback sensors combined with thermomechanical actuators for plant micromotion control systems
Simulation of motion of a three-link robot with controlled friction forces on a horizontal rough surface
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Kinematically optimal spacecraft attitude control

Content Provider Springer Nature Link
Author Levskii, M. V.
Copyright Year 2015
Abstract The problem of optimal control of a spacecraft reorientation from an arbitrary initial position into a prescribed final angular position is studied. The reorientation time is minimized. The case when the velocity parameters are limited is investigated. On the basis of necessary optimality conditions in the form of Pontryagin’s maximum principle and using quaternion variables for the control problems of the spacecraft motion, an analytical solution of the stated problem is obtained. The kinematic problem of spacecraft reorientation is solved completely. Formal equations are derived and computational expressions for constructing the optimal control program are obtained. For the symmetric form of constraints on the angular velocity vector, the optimal reorientation problem is solved analytically (the result is obtained in terms of elementary functions). Results of the mathematical simulation of the spacecraft motion under the optimal control are presented that demonstrate the practical usefulness of the proposed algorithm for the spacecraft attitude control.
Starting Page 116
Ending Page 132
Page Count 17
File Format PDF
ISSN 10642307
Journal Journal of Computer and Systems Sciences International
Volume Number 54
Issue Number 1
e-ISSN 15556530
Language English
Publisher Pleiades Publishing
Publisher Date 2015-02-13
Publisher Place Moscow
Access Restriction One Nation One Subscription (ONOS)
Subject Keyword Control, Robotics, Mechatronics
Content Type Text
Resource Type Article
Subject Applied Mathematics Theoretical Computer Science Computer Networks and Communications Control and Systems Engineering Information Systems Computer Vision and Pattern Recognition Software
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