TY - JOUR
T1 - Navigation strategy with the spacecraft communications blackout for Mars entry
AU - Wang, Xichen
AU - Xia, Yuanqing
N1 - Publisher Copyright:
© 2014 COSPAR. Published by Elsevier Ltd. All rights reserved.
PY - 2015/2/15
Y1 - 2015/2/15
N2 - Future Mars missions require precision entry navigation capability, especially in the presence of communications blackout. On the mission of Mars Science Laboratory (MSL), there was a 70-s communications blackout period during atmospheric entry phase. In allusion to the spacecraft communications blackout encountered, this paper predicts an upper-bound for any possible blackout period firstly, improves the default integrated navigation measurements based on IMU and surface radiometric beacons, and proposes innovative attitude observation model based on IMU and range observation model based on orbiters finally. To verify the accuracy and effectiveness of the proposed observation models in the presence of communications blackout, unscented Kalman filter is utilized to demonstrate the navigation performance. The results show that navigation errors based on improved observation models proposed in this paper degrade an order of magnitude compared with the default observation models even if the communications blackout takes place, which satisfies the requirements of future Mars landing missions.
AB - Future Mars missions require precision entry navigation capability, especially in the presence of communications blackout. On the mission of Mars Science Laboratory (MSL), there was a 70-s communications blackout period during atmospheric entry phase. In allusion to the spacecraft communications blackout encountered, this paper predicts an upper-bound for any possible blackout period firstly, improves the default integrated navigation measurements based on IMU and surface radiometric beacons, and proposes innovative attitude observation model based on IMU and range observation model based on orbiters finally. To verify the accuracy and effectiveness of the proposed observation models in the presence of communications blackout, unscented Kalman filter is utilized to demonstrate the navigation performance. The results show that navigation errors based on improved observation models proposed in this paper degrade an order of magnitude compared with the default observation models even if the communications blackout takes place, which satisfies the requirements of future Mars landing missions.
KW - Communications blackout
KW - IMU
KW - Integrated navigation
KW - Orbiters
UR - http://www.scopus.com/inward/record.url?scp=84921602803&partnerID=8YFLogxK
U2 - 10.1016/j.asr.2014.11.021
DO - 10.1016/j.asr.2014.11.021
M3 - Article
AN - SCOPUS:84921602803
SN - 0273-1177
VL - 55
SP - 1264
EP - 1277
JO - Advances in Space Research
JF - Advances in Space Research
IS - 4
ER -