Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying

This paper presents the application of a Modified State–Dependent Riccati Equation MSDRE approach in multi-object attitude and rate tracking. A nonlinear controller using the MSDRE is developed through a pseudo-linearization of spacecraft augmented nonlinear absolute dynamics and kinematics. The de...

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Main Author: Mohammad Abdelrahman, Mohammad Ibraheem
Format: Proceeding Paper
Language:English
Published: 2011
Subjects:
Online Access:http://irep.iium.edu.my/7304/1/AIAA-2011-6236-978.pdf
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author Mohammad Abdelrahman, Mohammad Ibraheem
author_facet Mohammad Abdelrahman, Mohammad Ibraheem
author_sort Mohammad Abdelrahman, Mohammad Ibraheem
collection IIUM
description This paper presents the application of a Modified State–Dependent Riccati Equation MSDRE approach in multi-object attitude and rate tracking. A nonlinear controller using the MSDRE is developed through a pseudo-linearization of spacecraft augmented nonlinear absolute dynamics and kinematics. The developed controller is adopted to solve a trajectory tracking/ model following problem. Based on the same approach the relative dynamics and kinematics are augmented to the previous system to represent the overall system process model. The developed controller is applied to spacecraft in formation as a decentralized control algorithm which aims to track absolute and relative attitude and rates simultaneously.The developed controller is applied to a spacecraft formation in a remote sensing mission.The simulations results show the capabilities of the MSDRE to handle the multi-object tracking without any unnecessary control efforts that might lead to actuators saturations or additional control logic to switch between absolute and relative tracking. Finally the stability of the controller is verified using Lyapunov function method.
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spelling oai:generic.eprints.org:73042011-12-28T00:53:09Z http://irep.iium.edu.my/7304/ Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying Mohammad Abdelrahman, Mohammad Ibraheem TL787 Astronautics This paper presents the application of a Modified State–Dependent Riccati Equation MSDRE approach in multi-object attitude and rate tracking. A nonlinear controller using the MSDRE is developed through a pseudo-linearization of spacecraft augmented nonlinear absolute dynamics and kinematics. The developed controller is adopted to solve a trajectory tracking/ model following problem. Based on the same approach the relative dynamics and kinematics are augmented to the previous system to represent the overall system process model. The developed controller is applied to spacecraft in formation as a decentralized control algorithm which aims to track absolute and relative attitude and rates simultaneously.The developed controller is applied to a spacecraft formation in a remote sensing mission.The simulations results show the capabilities of the MSDRE to handle the multi-object tracking without any unnecessary control efforts that might lead to actuators saturations or additional control logic to switch between absolute and relative tracking. Finally the stability of the controller is verified using Lyapunov function method. 2011 Proceeding Paper PeerReviewed application/pdf en http://irep.iium.edu.my/7304/1/AIAA-2011-6236-978.pdf Mohammad Abdelrahman, Mohammad Ibraheem (2011) Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying. In: AAIA Guidance, Navigation, and Control Conference, 8-11 August 2011, Portland, Oregon, USA.
spellingShingle TL787 Astronautics
Mohammad Abdelrahman, Mohammad Ibraheem
Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying
title Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying
title_full Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying
title_fullStr Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying
title_full_unstemmed Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying
title_short Multi-Object Attitude and Rate Tracking for Spacecraft in Formation Flying
title_sort multi object attitude and rate tracking for spacecraft in formation flying
topic TL787 Astronautics
url http://irep.iium.edu.my/7304/1/AIAA-2011-6236-978.pdf
work_keys_str_mv AT mohammadabdelrahmanmohammadibraheem multiobjectattitudeandratetrackingforspacecraftinformationflying