Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight

This paper presents a neural network assisted entry guidance law that is designed by applying Bézier approximation. It is shown that a fully constrained approximation of a reference trajectory can be made by using the Bézier curve. Applying this approximation, an inverse dynamic system for an entry...

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Main Authors: Hao Zhou, Tawfiqur Rahman, Wanchun Chen
Format: Article
Language:English
Published: Wiley 2014-01-01
Series:The Scientific World Journal
Online Access:http://dx.doi.org/10.1155/2014/686040
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author Hao Zhou
Tawfiqur Rahman
Wanchun Chen
author_facet Hao Zhou
Tawfiqur Rahman
Wanchun Chen
author_sort Hao Zhou
collection DOAJ
description This paper presents a neural network assisted entry guidance law that is designed by applying Bézier approximation. It is shown that a fully constrained approximation of a reference trajectory can be made by using the Bézier curve. Applying this approximation, an inverse dynamic system for an entry flight is solved to generate guidance command. The guidance solution thus gotten ensures terminal constraints for position, flight path, and azimuth angle. In order to ensure terminal velocity constraint, a prediction of the terminal velocity is required, based on which, the approximated Bézier curve is adjusted. An artificial neural network is used for this prediction of the terminal velocity. The method enables faster implementation in achieving fully constrained entry flight. Results from simulations indicate improved performance of the neural network assisted method. The scheme is expected to have prospect for further research on automated onboard control of terminal velocity for both reentry and terminal guidance laws.
format Article
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institution Kabale University
issn 2356-6140
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language English
publishDate 2014-01-01
publisher Wiley
record_format Article
series The Scientific World Journal
spelling doaj-art-b231f563135c48f5843b18851ed0471e2025-02-03T06:14:19ZengWileyThe Scientific World Journal2356-61401537-744X2014-01-01201410.1155/2014/686040686040Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry FlightHao Zhou0Tawfiqur Rahman1Wanchun Chen2School of Astronautics, Beihang University, Beijing 100191, ChinaSchool of Astronautics, Beihang University, Beijing 100191, ChinaSchool of Astronautics, Beihang University, Beijing 100191, ChinaThis paper presents a neural network assisted entry guidance law that is designed by applying Bézier approximation. It is shown that a fully constrained approximation of a reference trajectory can be made by using the Bézier curve. Applying this approximation, an inverse dynamic system for an entry flight is solved to generate guidance command. The guidance solution thus gotten ensures terminal constraints for position, flight path, and azimuth angle. In order to ensure terminal velocity constraint, a prediction of the terminal velocity is required, based on which, the approximated Bézier curve is adjusted. An artificial neural network is used for this prediction of the terminal velocity. The method enables faster implementation in achieving fully constrained entry flight. Results from simulations indicate improved performance of the neural network assisted method. The scheme is expected to have prospect for further research on automated onboard control of terminal velocity for both reentry and terminal guidance laws.http://dx.doi.org/10.1155/2014/686040
spellingShingle Hao Zhou
Tawfiqur Rahman
Wanchun Chen
Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight
The Scientific World Journal
title Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight
title_full Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight
title_fullStr Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight
title_full_unstemmed Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight
title_short Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight
title_sort neural network assisted inverse dynamic guidance for terminally constrained entry flight
url http://dx.doi.org/10.1155/2014/686040
work_keys_str_mv AT haozhou neuralnetworkassistedinversedynamicguidanceforterminallyconstrainedentryflight
AT tawfiqurrahman neuralnetworkassistedinversedynamicguidanceforterminallyconstrainedentryflight
AT wanchunchen neuralnetworkassistedinversedynamicguidanceforterminallyconstrainedentryflight