Spacecraft pose estimation and uncertainty modeling method based on intrinsic space
By constructing a probability distribution model in the rotation matrix manifold SO(3) and Euclidean space, using a hierarchical Bayesian framework to decouple uncertainties, and using an end-to-end neural network for spacecraft pose estimation, the problem of insufficient accuracy in complex space environments is solved, achieving high-precision and reliability assessment and improving the safety of autonomous decision-making.
Patent Information
- Application Number
- CN202610417516.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2026-04-01
- Publication Date
- 2026-06-19
- Estimated Expiration
- 2046-04-01
AI Technical Summary
Existing spacecraft attitude estimation methods lack accuracy in complex space environments and struggle to effectively distinguish between accidental uncertainties caused by observation noise and cognitive uncertainties caused by insufficient model knowledge, resulting in insufficient safety of autonomous decision-making.
A probability distribution model is constructed in the rotation matrix manifold SO(3) and Euclidean space. A hierarchical Bayesian framework is used to decouple random uncertainty and cognitive uncertainty. High-precision pose estimation and reliability quantification are achieved through an end-to-end neural network. Feature extraction and multi-task prediction are performed using EfficientNet and bidirectional feature pyramid network.
It improves the accuracy and stability of spacecraft attitude estimation, can clearly characterize the sources of uncertainty, provide reliable risk assessment basis, and enhance the safety of autonomous decision-making.