Mars Atmospheric Entry Integrated Navigation with Partial Intermittent Measurements
Signal degradation suffered by the vehicle is a combination brownout and blackout during Mars atmospheric entry. The communications brownout means that signal fades and blackout means that the signal is lost completely. The communications brownout and blackout periods are analyzed and predicted with...
Saved in:
Main Authors: | , , , |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2017-01-01
|
Series: | International Journal of Aerospace Engineering |
Online Access: | http://dx.doi.org/10.1155/2017/4378640 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
_version_ | 1832562595984310272 |
---|---|
author | Tai-shan Lou Yan Wang Guo-qiang Ding Liang-yu Zhao |
author_facet | Tai-shan Lou Yan Wang Guo-qiang Ding Liang-yu Zhao |
author_sort | Tai-shan Lou |
collection | DOAJ |
description | Signal degradation suffered by the vehicle is a combination brownout and blackout during Mars atmospheric entry. The communications brownout means that signal fades and blackout means that the signal is lost completely. The communications brownout and blackout periods are analyzed and predicted with an altitude and velocity profiles. In the brownout period, the range measurements between the vehicle and the orbiters are modeled as intermittent measurements with the radio signal arrival probabilities, which are distributed as a Rayleigh distribution of the electron number density around the entry vehicle. A new integrated navigation strategy during the Mars atmospheric entry phase is proposed to consider the probabilities of the radio measurements in the communications brownout and blackout periods under the IMU/beacon scenario based on the information filter with intermittent measurements. Numerical navigation simulations are designed to show the performance of the proposed navigation strategy under the integrated navigation scenario. |
format | Article |
id | doaj-art-3ebe298f4ed84e3881dfa6a750d42cb9 |
institution | Kabale University |
issn | 1687-5966 1687-5974 |
language | English |
publishDate | 2017-01-01 |
publisher | Wiley |
record_format | Article |
series | International Journal of Aerospace Engineering |
spelling | doaj-art-3ebe298f4ed84e3881dfa6a750d42cb92025-02-03T01:22:11ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742017-01-01201710.1155/2017/43786404378640Mars Atmospheric Entry Integrated Navigation with Partial Intermittent MeasurementsTai-shan Lou0Yan Wang1Guo-qiang Ding2Liang-yu Zhao3School of Electrical and Information Engineering, Zhengzhou University of Light Industry, Zhengzhou 45002, ChinaSchool of Electrical and Information Engineering, Zhengzhou University of Light Industry, Zhengzhou 45002, ChinaSchool of Electrical and Information Engineering, Zhengzhou University of Light Industry, Zhengzhou 45002, ChinaSchool of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, ChinaSignal degradation suffered by the vehicle is a combination brownout and blackout during Mars atmospheric entry. The communications brownout means that signal fades and blackout means that the signal is lost completely. The communications brownout and blackout periods are analyzed and predicted with an altitude and velocity profiles. In the brownout period, the range measurements between the vehicle and the orbiters are modeled as intermittent measurements with the radio signal arrival probabilities, which are distributed as a Rayleigh distribution of the electron number density around the entry vehicle. A new integrated navigation strategy during the Mars atmospheric entry phase is proposed to consider the probabilities of the radio measurements in the communications brownout and blackout periods under the IMU/beacon scenario based on the information filter with intermittent measurements. Numerical navigation simulations are designed to show the performance of the proposed navigation strategy under the integrated navigation scenario.http://dx.doi.org/10.1155/2017/4378640 |
spellingShingle | Tai-shan Lou Yan Wang Guo-qiang Ding Liang-yu Zhao Mars Atmospheric Entry Integrated Navigation with Partial Intermittent Measurements International Journal of Aerospace Engineering |
title | Mars Atmospheric Entry Integrated Navigation with Partial Intermittent Measurements |
title_full | Mars Atmospheric Entry Integrated Navigation with Partial Intermittent Measurements |
title_fullStr | Mars Atmospheric Entry Integrated Navigation with Partial Intermittent Measurements |
title_full_unstemmed | Mars Atmospheric Entry Integrated Navigation with Partial Intermittent Measurements |
title_short | Mars Atmospheric Entry Integrated Navigation with Partial Intermittent Measurements |
title_sort | mars atmospheric entry integrated navigation with partial intermittent measurements |
url | http://dx.doi.org/10.1155/2017/4378640 |
work_keys_str_mv | AT taishanlou marsatmosphericentryintegratednavigationwithpartialintermittentmeasurements AT yanwang marsatmosphericentryintegratednavigationwithpartialintermittentmeasurements AT guoqiangding marsatmosphericentryintegratednavigationwithpartialintermittentmeasurements AT liangyuzhao marsatmosphericentryintegratednavigationwithpartialintermittentmeasurements |