Nonlinear stochastic evaluation of the orientation parameters of a strapdown inertial navigation system of a space vehicle during prelaunch preparation
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Publication:2134324
DOI10.1134/S1064230721060083zbMath1490.93119OpenAlexW4200565398MaRDI QIDQ2134324
Publication date: 3 May 2022
Published in: Journal of Computer and Systems Sciences International (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1134/s1064230721060083
Filtering in stochastic control theory (93E11) Estimation and detection in stochastic control theory (93E10)
Cites Work
- A problem of satellite orientation determination by spaced satellite antennas and angular rate sensors
- In-flight alignment of a strapdown inertial navigation system of an unmanned aerial vehicle
- Algorithmic support for integrated navigation systems
- On the rapid orbital attitude control of manned and cargo spacecraft \textit{Soyuz MS} and \textit{Progress MS}
- Nonlinear Complementary Filters on the Special Orthogonal Group
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