Title of article
Near optimal guidance law for descent to a point using inverse problem approach
Author/Authors
Naghash، نويسنده , , Abolghasem and Esmaelzadeh، نويسنده , , Reza and Mortazavi، نويسنده , , Mehdi and Jamilnia، نويسنده , , Reza، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2008
Pages
7
From page
241
To page
247
Abstract
An explicit guidance law that maximizes terminal velocity is developed for a reentry vehicle to a fixed target. Motion is constrained to an optimal, three-dimensional Bezier curve. Acceleration commands are derived by solving an inverse problem related to Bezier parameters. An optimal Bezier curve is determined by solving a real-coded genetic algorithm. For online trajectory generation, optimal trajectory is approximated by fixing the second control point of the Bezier curve. The approximated trajectory is compared with the pure proportional navigation, genetic algorithm and direct transcriptionʹs solutions. The near optimal terminal velocity solution compares very well with these solutions. The approach robustness is examined by Monte Carlo simulation.
Keywords
Explicit guidance , Optimal guidance , genetic algorithm , Bezier curve , Reentry
Journal title
Aerospace Science and Technology
Serial Year
2008
Journal title
Aerospace Science and Technology
Record number
2229750
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