TY - JOUR
T1 - On the observability of Mars entry navigation using radiometric measurements
AU - Yu, Zhengshi
AU - Cui, Pingyuan
AU - Zhu, Shengying
N1 - Publisher Copyright:
© 2014 COSPAR. Published by Elsevier Ltd. All rights reserved.
PY - 2014
Y1 - 2014
N2 - A thorough observability analysis of the Mars entry navigation using radiometric measurements from ground based beacons is performed. This analysis involves the evaluation of the Fisher information matrix which is derived from the maximum likelihood estimation. A series of navigation cases with multiple beacons are investigated, and both range and range-rate measurements are considered. The determinant of Fisher information matrix is used to quantify the observability of navigation system, while the trace of Fisher information matrix is used to determine the lower-bound of estimation errors. For one and two beacon cases, the navigation system is unobservable. However, the eigenvectors of Fisher information matrix give the observable and unobservable component. When three or more beacon measurements are employed, the states of entry vehicle become observable. Some valuable analytic conclusions on the relationship between the geometric configuration of beacons and observability are obtained consequently. Finally, simulation results from two navigation examples indicate that our effort is useful for understanding and assessing the observability of the Mars entry navigation using radiometric measurements.
AB - A thorough observability analysis of the Mars entry navigation using radiometric measurements from ground based beacons is performed. This analysis involves the evaluation of the Fisher information matrix which is derived from the maximum likelihood estimation. A series of navigation cases with multiple beacons are investigated, and both range and range-rate measurements are considered. The determinant of Fisher information matrix is used to quantify the observability of navigation system, while the trace of Fisher information matrix is used to determine the lower-bound of estimation errors. For one and two beacon cases, the navigation system is unobservable. However, the eigenvectors of Fisher information matrix give the observable and unobservable component. When three or more beacon measurements are employed, the states of entry vehicle become observable. Some valuable analytic conclusions on the relationship between the geometric configuration of beacons and observability are obtained consequently. Finally, simulation results from two navigation examples indicate that our effort is useful for understanding and assessing the observability of the Mars entry navigation using radiometric measurements.
KW - Fisher information matrix
KW - Geometric configuration
KW - Mars entry navigation
KW - Observability
KW - Radiometric measurements
UR - http://www.scopus.com/inward/record.url?scp=84922584979&partnerID=8YFLogxK
U2 - 10.1016/j.asr.2014.06.036
DO - 10.1016/j.asr.2014.06.036
M3 - Article
AN - SCOPUS:84922584979
SN - 0273-1177
VL - 54
SP - 1513
EP - 1524
JO - Advances in Space Research
JF - Advances in Space Research
IS - 8
ER -