Relative navigation of fixed-wing aircraft in GPS-denied environments

Gary Ellingson, Kevin Brink, Tim McLain

Peer Reviewed

Abstract: This work enables GPS-denied flight on fixed-wing UAS by accounting for fixed-wing-specific sensing requirements and using a methodology called relative navigation as an overarching framework. The development of an odometry-like, front-end, EKF-based estimator that utilizes only a monocular camera and an inertial measurement unit (IMU) is presented. The filter uses the measurement model of the multi-state-constraint Kalman filter. The filter also regularly resets its origin in coordination with the declaration of keyframe images. The keyframe-to-keyframe odometry estimates and their covariances are sent to a global back end that represents the global state as a pose graph. The back end is better suited to represent nonlinear uncertainties and incorporate opportunistic global constraints.We also introduce a method to account for front-end velocity bias in the back-end optimization. The paper provides simulation and hardware flight-test results of the front-end estimator and performs several back-end optimizations on the front-end data.
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Published in: NAVIGATION, Journal of the Institute of Navigation, Volume 67, Number 2
Pages: 255 - 273
Cite this article: Export Citation
https://doi.org/10.1002/navi.364
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