Abstract
This paper presents an ℓ1-regularized optimization based technique which effectively eliminates the optical misalignment effects encountered in the squint guidance mode with strapdown seekers. We formulated a series of ℓ1-regularized optimization problems in order to separate the bias and the gradient components from the measured data, and solved it via the alternating direction method of multipliers and sparse matrix decomposition techniques. The proposed technique was able to rapidly detect arbitrary discontinuities and gradient changes from the measured signals, and was shown to effectively cancel the undesirable effects coming from the seeker’s optical misalignment.
Original language | English |
---|---|
Pages (from-to) | 711-717 |
Number of pages | 7 |
Journal | International Journal of Aeronautical and Space Sciences |
Volume | 19 |
Issue number | 3 |
DOIs | |
Publication status | Published - 1 Sept 2018 |
Bibliographical note
Publisher Copyright:© 2018, The Korean Society for Aeronautical & Space Sciences and Springer Nature Singapore Pte Ltd.
Keywords
- Convex optimization
- Seeker misalignment cancellation
- ℓ-regularized optimization