Optimal trajectory tracking using an output feedback preview controller

This paper investigates the use of preview control for optimal trajectory tracking for air-to-surface missiles. An off-line reference trajectory is obtained by solving a trajectory optimisation problem that incorporates the mission constraints. A trajectory following guidance scheme using a preview...

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Bibliographic Details
Main Authors: Farooq, A, MacBean, P, Limebeer, D
Format: Journal article
Language:English
Published: 2006