TY - GEN
T1 - Estimating attitude from signal-to-noise ratio at multiple ground-based receivers
AU - Pimienta-Peñalver, Adonis
AU - Crassidis, John L.
N1 - Publisher Copyright:
© 2019 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2019
Y1 - 2019
N2 - This paper presents the implementation of an attitude estimation algorithm to be applied in multiple space-or Earth-based receiver platforms using signal-to-noise ratio from received transmissions from a single broadcasting satellite. A statistical method based on received signal samples is applied to estimate the incoming signal-to-noise ratio, which then facilitates the geometrical derivation of line-of-sight and boresight pointing estimates using geometric relations. The results of this deterministic approach show that at least three independent receivers with non-collinear lines-of-sight are necessary to obtain a three-dimensional boresight solution. Furthermore, an observability study is carried out along with sequential estimation for attitude/maneuver detection. Results indicate a dependence on a-priori knowledge of the bradcaster’s RF characteristics, as well the viability of estimating attitude via signal-to-noise ratio as a complement to additional space situational awareness approaches.
AB - This paper presents the implementation of an attitude estimation algorithm to be applied in multiple space-or Earth-based receiver platforms using signal-to-noise ratio from received transmissions from a single broadcasting satellite. A statistical method based on received signal samples is applied to estimate the incoming signal-to-noise ratio, which then facilitates the geometrical derivation of line-of-sight and boresight pointing estimates using geometric relations. The results of this deterministic approach show that at least three independent receivers with non-collinear lines-of-sight are necessary to obtain a three-dimensional boresight solution. Furthermore, an observability study is carried out along with sequential estimation for attitude/maneuver detection. Results indicate a dependence on a-priori knowledge of the bradcaster’s RF characteristics, as well the viability of estimating attitude via signal-to-noise ratio as a complement to additional space situational awareness approaches.
UR - https://www.scopus.com/pages/publications/85083944264
U2 - 10.2514/6.2019-0375
DO - 10.2514/6.2019-0375
M3 - Conference contribution
AN - SCOPUS:85083944264
SN - 9781624105784
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -