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Relative motion guidance, navigation and control for autonomous orbital rendezvous

In this paper, the dynamics of the relative motion problem in a perturbed orbital environment are exploited based on Gauss’ variational equations. The relative coordinate frame (Hill frame) is studied to describe the relative motion. A linear high fidelity model is developed to describe the relative...

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Main Authors: Okasha, Mohamed Elsayed Aly Abd Elaziz, Newman, Brett
Format: Article
Language:English
English
Published: Instituto de Aeronautica e Espaco-IAE - Brazil 2014
Subjects:
TA168 Systems engineering
TA329 Engineering mathematics. Engineering analysis
TA349 Mechanics of engineering. Applied mechanics
TJ212 Control engineering
Online Access:http://irep.iium.edu.my/38405/1/38405_Relative%20motion%20guidance%2C%20navigation.pdf
http://irep.iium.edu.my/38405/2/38405_Relative%20motion%20guidance%2C%20navigation_SCOPUS.pdf
http://irep.iium.edu.my/38405/
http://www.jatm.com.br/ojs/index.php/jatm/article/view/330
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spelling my.iium.irep.384052017-09-26T07:58:33Z http://irep.iium.edu.my/38405/ Relative motion guidance, navigation and control for autonomous orbital rendezvous Okasha, Mohamed Elsayed Aly Abd Elaziz Newman, Brett TA168 Systems engineering TA329 Engineering mathematics. Engineering analysis TA349 Mechanics of engineering. Applied mechanics TJ212 Control engineering In this paper, the dynamics of the relative motion problem in a perturbed orbital environment are exploited based on Gauss’ variational equations. The relative coordinate frame (Hill frame) is studied to describe the relative motion. A linear high fidelity model is developed to describe the relative motion. This model takes into account primary gravitational and atmospheric drag perturbations. In addition, this model is used in the design of a control, guidance, and navigation system of a chaser vehicle to approach towards and to depart from a target vehicle in proximity operations. Relative navigation uses an extended Kalman filter based on this relative model to estimate the relative position and velocity of the chaser vehicle with respect to the target vehicle and the chaser attitude and gyros biases. This filter uses the range and angle measurements of the target relative to the chaser from a simulated Light Detection and Ranging (LIDAR) system, along with the star tracker and gyro measurements of the chaser. The corresponding measurement models, process noise matrix and other filter parameters are provided. Numerical simulations are performed to assess the precision of this model with respect to the full nonlinear model.The analyses include the navigations errors, trajectory dispersions, and attitude dispersions. Instituto de Aeronautica e Espaco-IAE - Brazil 2014-07 Article REM application/pdf en http://irep.iium.edu.my/38405/1/38405_Relative%20motion%20guidance%2C%20navigation.pdf application/pdf en http://irep.iium.edu.my/38405/2/38405_Relative%20motion%20guidance%2C%20navigation_SCOPUS.pdf Okasha, Mohamed Elsayed Aly Abd Elaziz and Newman, Brett (2014) Relative motion guidance, navigation and control for autonomous orbital rendezvous. Journal of Aerospace Technology and Management, 6 (3). pp. 301-318. ISSN 1984-9648 http://www.jatm.com.br/ojs/index.php/jatm/article/view/330 10.5028/jatm.v6i3.330
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TA168 Systems engineering
TA329 Engineering mathematics. Engineering analysis
TA349 Mechanics of engineering. Applied mechanics
TJ212 Control engineering
spellingShingle TA168 Systems engineering
TA329 Engineering mathematics. Engineering analysis
TA349 Mechanics of engineering. Applied mechanics
TJ212 Control engineering
Okasha, Mohamed Elsayed Aly Abd Elaziz
Newman, Brett
Relative motion guidance, navigation and control for autonomous orbital rendezvous
description In this paper, the dynamics of the relative motion problem in a perturbed orbital environment are exploited based on Gauss’ variational equations. The relative coordinate frame (Hill frame) is studied to describe the relative motion. A linear high fidelity model is developed to describe the relative motion. This model takes into account primary gravitational and atmospheric drag perturbations. In addition, this model is used in the design of a control, guidance, and navigation system of a chaser vehicle to approach towards and to depart from a target vehicle in proximity operations. Relative navigation uses an extended Kalman filter based on this relative model to estimate the relative position and velocity of the chaser vehicle with respect to the target vehicle and the chaser attitude and gyros biases. This filter uses the range and angle measurements of the target relative to the chaser from a simulated Light Detection and Ranging (LIDAR) system, along with the star tracker and gyro measurements of the chaser. The corresponding measurement models, process noise matrix and other filter parameters are provided. Numerical simulations are performed to assess the precision of this model with respect to the full nonlinear model.The analyses include the navigations errors, trajectory dispersions, and attitude dispersions.
format Article
author Okasha, Mohamed Elsayed Aly Abd Elaziz
Newman, Brett
author_facet Okasha, Mohamed Elsayed Aly Abd Elaziz
Newman, Brett
author_sort Okasha, Mohamed Elsayed Aly Abd Elaziz
title Relative motion guidance, navigation and control for autonomous orbital rendezvous
title_short Relative motion guidance, navigation and control for autonomous orbital rendezvous
title_full Relative motion guidance, navigation and control for autonomous orbital rendezvous
title_fullStr Relative motion guidance, navigation and control for autonomous orbital rendezvous
title_full_unstemmed Relative motion guidance, navigation and control for autonomous orbital rendezvous
title_sort relative motion guidance, navigation and control for autonomous orbital rendezvous
publisher Instituto de Aeronautica e Espaco-IAE - Brazil
publishDate 2014
url http://irep.iium.edu.my/38405/1/38405_Relative%20motion%20guidance%2C%20navigation.pdf
http://irep.iium.edu.my/38405/2/38405_Relative%20motion%20guidance%2C%20navigation_SCOPUS.pdf
http://irep.iium.edu.my/38405/
http://www.jatm.com.br/ojs/index.php/jatm/article/view/330
_version_ 1643611418516258816
score 13.211869

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