Abstract

For navigation on asteroid surface, optimizing jointly a set of system states over a collection of measurements is an alternative to filtering-based state estimators. In order to investigate the feasibility of a sliding window smoother for the task of state estimation in exploration on the asteroid terrain surface, we propose an optimization-based relative flash LiDAR aided-inertial navigation algorithm. The local relative navigation framework is chosen for locally drift-free state estimation accounting for relative state observations from registration of flash LiDAR point clouds. State constraints derived from the point cloud registration and IMU pre-integration are leveraged in the optimization. Simulation-based validation in a high fidelity simulated environment shows that the proposed optimization-based local relative navigation is capable of estimating spacecraft system states accurately with acceptable computation complexity in our application cases.

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.