Pulsar navigation for interplanetary missions using CV model and ASUKF
Pulsar navigation for interplanetary missions using CV model and ASUKF
To improve the navigation performance with the pulsar direction error and the clock error, X-ray pulsar navigation for interplanetary missions is proposed. We analyze the clock error and the system bias caused by the pulsar direction error, and find that the system bias is large but the bias’ variation velocity and the clock frequency error within a short time can be viewed as constants. Thus, both the bias and clock error can be modeled as the constant velocity (CV) model, and the augmented state unscented Kalman filter (ASUKF) is utilized here to deal with them and estimate the spacecraft’s positions. The simulation results demonstrate that the proposed method can improve the navigation accuracy in the presence of the clock error and the pulsar direction error.
19-23
Lui, J.
5d26c472-fbd5-4bdc-980a-d03851363797
Jie, M.
7dba82b4-177e-4a96-855b-2263f5b645a7
Kang, Z.
eccfb1ea-9864-4ae7-ba4a-ee39d0413b17
White, P.R.
2dd2477b-5aa9-42e2-9d19-0806d994eaba
November 2012
Lui, J.
5d26c472-fbd5-4bdc-980a-d03851363797
Jie, M.
7dba82b4-177e-4a96-855b-2263f5b645a7
Kang, Z.
eccfb1ea-9864-4ae7-ba4a-ee39d0413b17
White, P.R.
2dd2477b-5aa9-42e2-9d19-0806d994eaba
Lui, J., Jie, M., Kang, Z. and White, P.R.
(2012)
Pulsar navigation for interplanetary missions using CV model and ASUKF.
Aerospace Science and Technology, 22 (1), .
(doi:10.1016/j.ast.2011.04.010).
Abstract
To improve the navigation performance with the pulsar direction error and the clock error, X-ray pulsar navigation for interplanetary missions is proposed. We analyze the clock error and the system bias caused by the pulsar direction error, and find that the system bias is large but the bias’ variation velocity and the clock frequency error within a short time can be viewed as constants. Thus, both the bias and clock error can be modeled as the constant velocity (CV) model, and the augmented state unscented Kalman filter (ASUKF) is utilized here to deal with them and estimate the spacecraft’s positions. The simulation results demonstrate that the proposed method can improve the navigation accuracy in the presence of the clock error and the pulsar direction error.
This record has no associated files available for download.
More information
Published date: November 2012
Organisations:
Signal Processing & Control Grp
Identifiers
Local EPrints ID: 353131
URI: http://eprints.soton.ac.uk/id/eprint/353131
ISSN: 1270-9638
PURE UUID: 0c8837c0-94fc-4586-b74c-acca993b4748
Catalogue record
Date deposited: 30 May 2013 13:30
Last modified: 11 Jul 2024 01:33
Export record
Altmetrics
Contributors
Author:
J. Lui
Author:
M. Jie
Author:
Z. Kang
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.
View more statistics