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A Settling Time Constrained Optimization of a Velocity Inertial Navigation System

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2 Author(s)
W. A. Porter ; The Control Systems Research Unit of the Institute of Science and Technology, The University of Michigan, Ann Arbor, Mich. ; M. C. Y. Kuo

In this paper, a description of a technique for improving transient performance in the velocity inertial system while minimizing the standard deviation of the system error, (i.e., standard deviation of the system velocity measurement error ¿v2) is given. To accomplish this objective, a prescribed settling time constraint is formulated for the system response. The constraint equation is then imposed on the minimization process. The result shows that considerable settling time improvement can be derived without sacrificing system accuracy.

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IEEE Transactions on Aerospace and Navigational Electronics  (Volume:ANE-11 ,  Issue: 2 )