Minimum Time Ascent Phase Trajectory Optimization using Steepest Descent Method

Singh, Diksha Diva and Nair, Vishnu G and Dileep, M V (2016) Minimum Time Ascent Phase Trajectory Optimization using Steepest Descent Method. International Journal of Control Theory and Applications, 9 (39). pp. 71-76. ISSN 09745572

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Abstract

In this paper, ascent phase gravity turn trajectory of a launch vehicle is taken into account. Minimum-time problem of optimization is considered for specifi ed structural and propulsive data. The objective is to achieve the target in minimum time and minimum error at terminal point by taking into account all the constraints. Trajectory generation is done for a single stage rocket in 2-D plane and computed for a given initial and fi nal conditions. Hamiltonian is formulated by converting the given problem into secure fi nal fl ight path angle problem and Pontryagin minimum principle is used to fi nd the necessary conditions. The non-linear equations are solved using gradient method. Ultimately, the numerical results are evaluated and validity of result is exhibited.

Item Type: Article
Uncontrolled Keywords: Varying Inertia Weight; Trajectory Optimization; Minimum time.
Subjects: Engineering > MIT Manipal > Aeronautical and Automobile
Depositing User: MIT Library
Date Deposited: 07 Jan 2017 10:17
Last Modified: 07 Jan 2017 10:17
URI: http://eprints.manipal.edu/id/eprint/147917

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