Expected Attitude Angle Design for Spacecraft Multi-target Tracking

DOI

10.2991/iccnce.2013.113How to use a DOI?

Keywords

Fixed Antenna, Installation Angle Design, Multi-target Tracking, Expected Attitude Angle

Abstract

This paper studies the spacecraft multi-target tracking. Firstly, the spacecraft expected attitude angle is designed according to the mission requirement, namely having the camera on the chaser spacecraft point strictly to the target spacecraft and maximizing the communication time between the antenna on the chaser spacecraft and the Earth. Then, the appropriate antenna installation angle is calculated based on task constraints. Finally, numerical simulation is presented to verify the effectiveness of the design of expected attitude angle and antenna installation angle.

Copyright

© 2013, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Yao Zhang
AU  - Wei Liu
AU  - Jingrui Zhang
PY  - 2013/07
DA  - 2013/07
TI  - Expected Attitude Angle Design for Spacecraft Multi-target Tracking
BT  - Proceedings of the International Conference on Computer, Networks and Communication Engineering (ICCNCE 2013)
PB  - Atlantis Press
SP  - 450
EP  - 454
SN  - 1951-6851
UR  - https://doi.org/10.2991/iccnce.2013.113
DO  - 10.2991/iccnce.2013.113
ID  - Zhang2013/07
ER  -