Inverse Kinematics of an Untethered Rigid Body Undergoing a Sequence of Forward and Reverse Rotations

Author:

Koh Sung K.1,Ananthasuresh G. K.1

Affiliation:

1. Department of Mechanical Engineering and Applied Mechanics, University of Pennsylvania, Philadelphia, PA 19104

Abstract

A sequence of rotations considered in this paper is a series of rotations of an untethered rigid body about its body-fixed axes such that the rotation about each axis is fully reversed at the end of the sequence. Due to the noncommutative property of finite rigid body rotations, such a sequence can effect nonzero changes in the orientation of the rigid body even though the net rotation about each axis is zero. These sequences are useful for attitude maneuvers of miniature spacecraft that use elastic deformation-based microactuators, or of other airborne or neutrally buoyant underwater vehicles. This paper considers the inverse kinematics problem of determining the angles in a given sequence to achieve a desired change in the orientation. Two types of problems are addressed. For the first problem, where four-rotation sequences are used, an analytical solution is presented and it is shown that a pointing vector attached to the rigid-body can be arbitrarily oriented. In the second problem, six-rotation sequences are used to control all three of the orientation freedoms of the rigid body. Some of the six-rotation sequences can provide any change in orientation while others are limited in their capabilities. A general numerical solution for all types, and a closed-form analytical solution for one type are presented along with the numerical examples and graphical visualization.

Publisher

ASME International

Subject

Computer Graphics and Computer-Aided Design,Computer Science Applications,Mechanical Engineering,Mechanics of Materials

Reference13 articles.

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2. Fleeter, R., 1995, Micro Spacecraft, The Edge City Press, Reston, VA.

3. Reiter, J., Bo¨hringer, K., and Campbell, M., 1999, “MEMS Control Moment Gyroscope Design and Wafer-Based Spacecraft Chassis Study,” SPIE Symposium on Micromachining and Microfabrication, Santa Clara, CA, September, 1999.

4. Li, J., Koh, S. K., Ananthasuresh, G. K., Ayyaswamy, P. S., and Ananthakrishnan, S., 2001, “A Novel Attitude Control Technique for Miniature Spacecraft,” MEMS Symposium, Vol. 1 CD-ROM Proceedings of 2001 ASME International Mechanical Engineering Conference and Exposition, November 11–16, 2001, New York.

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