Robust Angles-Only Initial Relative Orbit Determination Using Polynomial Optimization

Fuente: arXiv
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Hauptverfasser: Zhou, Xingyu, Macdonald, Malcolm, Armellin, Roberto, Qiao, Dong, Li, Xiangyu
Format: Preprint
Veröffentlicht: 2026
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author Zhou, Xingyu
Macdonald, Malcolm
Armellin, Roberto
Qiao, Dong
Li, Xiangyu
author_facet Zhou, Xingyu
Macdonald, Malcolm
Armellin, Roberto
Qiao, Dong
Li, Xiangyu
contents This paper develops a robust angles-only IROD method based on polynomial optimization for arbitrary nonlinear dynamics. First, the relative motion is approximated by high-order Taylor polynomials within the differential algebra framework, and the resulting cross-product-residual minimization problem is solved through a recursive polynomial optimization procedure. Second, a reduced-order weighting strategy is introduced by projecting the residual onto the two-dimensional tangent subspace of the line of sight, thereby structurally removing the intrinsic singularity of conventional three-dimensional weighting. Third, a zero-solution-avoidance constraint together with an adaptive threshold-selection mechanism is developed to improve robustness against poor initialization, strong measurement noise, and unfavorable observation geometries. Numerical simulations show that the proposed method improves IROD accuracy by about three orders of magnitude relative to the baseline methods, while also reducing the downstream orbit-refinement burden. The reduced-order weighting strategy further improves accuracy by about 43% in the nominal case and remains stable under large-noise conditions, outperforming the conventional three-dimensional weighting by about 81%.
format Preprint
id arxiv_https___arxiv_org_abs_2604_24451
institution arXiv
publishDate 2026
record_format arxiv
spellingShingle Robust Angles-Only Initial Relative Orbit Determination Using Polynomial Optimization
Zhou, Xingyu
Macdonald, Malcolm
Armellin, Roberto
Qiao, Dong
Li, Xiangyu
Instrumentation and Methods for Astrophysics
This paper develops a robust angles-only IROD method based on polynomial optimization for arbitrary nonlinear dynamics. First, the relative motion is approximated by high-order Taylor polynomials within the differential algebra framework, and the resulting cross-product-residual minimization problem is solved through a recursive polynomial optimization procedure. Second, a reduced-order weighting strategy is introduced by projecting the residual onto the two-dimensional tangent subspace of the line of sight, thereby structurally removing the intrinsic singularity of conventional three-dimensional weighting. Third, a zero-solution-avoidance constraint together with an adaptive threshold-selection mechanism is developed to improve robustness against poor initialization, strong measurement noise, and unfavorable observation geometries. Numerical simulations show that the proposed method improves IROD accuracy by about three orders of magnitude relative to the baseline methods, while also reducing the downstream orbit-refinement burden. The reduced-order weighting strategy further improves accuracy by about 43% in the nominal case and remains stable under large-noise conditions, outperforming the conventional three-dimensional weighting by about 81%.
title Robust Angles-Only Initial Relative Orbit Determination Using Polynomial Optimization
topic Instrumentation and Methods for Astrophysics
url https://arxiv.org/abs/2604.24451