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Simplex Back Propagation Estimation Method for Out-of-Sequence Attitude Sensor Measurements.

Shu Ting Goh1, M S C Tissera1, RongDe Darius Tan1

  • 1Department of Electrical & Computer Engineering, National University of Singapore, Singapore 117583, Singapore.

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|October 27, 2022
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Summary

A new simplex-back-propagation Kalman filter (SBPKF) improves attitude estimation accuracy for small satellites by addressing asynchronous data issues. This method offers superior performance and reduced computational load compared to existing filters.

Keywords:
Kalman filterattitude estimationout-of-sequence measurementsmall satellite

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Area of Science:

  • Aerospace Engineering
  • Control Systems
  • Satellite Technology

Background:

  • Small satellite attitude determination and control systems (ADCS) processors face challenges with asynchronous data acquisition from sensors and actuators.
  • This data asynchronicity degrades the accuracy of traditional attitude estimation methods like the extended Kalman filter (EKF), which assume synchronous data.

Purpose of the Study:

  • To develop a novel Kalman filter algorithm that minimizes attitude estimation accuracy loss caused by asynchronous data in small satellites.
  • To ensure the proposed algorithm maintains reasonable computational complexity suitable for resource-constrained small satellite applications.

Main Methods:

  • Proposes the simplex-back-propagation Kalman filter (SBPKF), which integrates time delay, gyro instability, and navigation error into measurement and covariance estimation.
  • Compares SBPKF performance against extended Kalman filter (EKF), modified adaptive EKF (MAEKF), and moving-covariance Kalman filter (MC-KF) through simulations.

Main Results:

  • SBPKF demonstrates at least a 30% reduction in attitude estimation error compared to EKF and MC-KF.
  • SBPKF exhibits 17% lower computational complexity than MAEKF and 29% lower than MC-KF.

Conclusions:

  • The simplex-back-propagation Kalman filter (SBPKF) effectively mitigates accuracy degradation from asynchronous data in small satellite ADCS.
  • SBPKF offers a computationally efficient and accurate solution for attitude determination in small satellite applications.