Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection
To estimate a spacecraft trajectory, the observation satellite position should be calculated in advance. Through the simplified equation of motion based on the observation satellite for finishing the second order differential equation. By the MATLAB simulation interpolation operation with the existi...
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doaj-4ed58547b461463e82461b787a4410392020-11-24T23:21:09ZengIFSA Publishing, S.L.Sensors & Transducers2306-85151726-54792014-12-0118312184191Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection ZHOU Juan0ZHONG Maosheng1School of Software, East China Jiaotong University, Nanchang, 330013, China School of Information Engineering, East China Jiaotong University, Nanchang, 330013, ChinaTo estimate a spacecraft trajectory, the observation satellite position should be calculated in advance. Through the simplified equation of motion based on the observation satellite for finishing the second order differential equation. By the MATLAB simulation interpolation operation with the existing list data, solution to satellite of three dimensional position in different moments. By the point wise intersection positioning method to estimating the trajectory of the spacecraft, the position and velocity of the spacecraft in a certain time will be obtained. And using simulated annealing for the mathematical model of a spacecraft trajectory and analyzing the rationality of the estimate.http://www.sensorsportal.com/HTML/DIGEST/december_2014/Vol_183/P_2561.pdfMATLAB interpolationPoint wise intersection positioning methodTrajectory reckonSimulated annealing. |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
ZHOU Juan ZHONG Maosheng |
spellingShingle |
ZHOU Juan ZHONG Maosheng Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection Sensors & Transducers MATLAB interpolation Point wise intersection positioning method Trajectory reckon Simulated annealing. |
author_facet |
ZHOU Juan ZHONG Maosheng |
author_sort |
ZHOU Juan |
title |
Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection |
title_short |
Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection |
title_full |
Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection |
title_fullStr |
Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection |
title_full_unstemmed |
Estimation about Active Phase of Trajectory Based on the Satellite Passive Detection |
title_sort |
estimation about active phase of trajectory based on the satellite passive detection |
publisher |
IFSA Publishing, S.L. |
series |
Sensors & Transducers |
issn |
2306-8515 1726-5479 |
publishDate |
2014-12-01 |
description |
To estimate a spacecraft trajectory, the observation satellite position should be calculated in advance. Through the simplified equation of motion based on the observation satellite for finishing the second order differential equation. By the MATLAB simulation interpolation operation with the existing list data, solution to satellite of three dimensional position in different moments. By the point wise intersection positioning method to estimating the trajectory of the spacecraft, the position and velocity of the spacecraft in a certain time will be obtained. And using simulated annealing for the mathematical model of a spacecraft trajectory and analyzing the rationality of the estimate. |
topic |
MATLAB interpolation Point wise intersection positioning method Trajectory reckon Simulated annealing. |
url |
http://www.sensorsportal.com/HTML/DIGEST/december_2014/Vol_183/P_2561.pdf |
work_keys_str_mv |
AT zhoujuan estimationaboutactivephaseoftrajectorybasedonthesatellitepassivedetection AT zhongmaosheng estimationaboutactivephaseoftrajectorybasedonthesatellitepassivedetection |
_version_ |
1725572559428124672 |