Publication | Open Access
Efficient and Optimal Attitude Determination Using Recursive Global Positioning System Signal Operations
53
Citations
18
References
1999
Year
EngineeringLocation EstimationGlobal Navigation Satellite SystemPositioning SystemSpacecraft Attitude ControlLocalizationState EstimationNonlinear System IdentificationCalibrationSystems EngineeringPositioningKinematicsTracking ControlAutomatic NavigationMechatronicsComputer EngineeringDynamic PositioningCoplanar Baseline ConfigurationsNew AlgorithmSignal ProcessingDynamic Hardware SimulatorOdometryAerospace Engineering
In this paper, a new and efficient algorithm is developed for attitude determination from Global Positioning System signals. The new algorithm is derived from a generalized nonlinear predictive filter for nonlinear systems. This uses a one time-step ahead approach to propagate a simple kinematics model for attitude determination. The advantages of the new algorithm over previously developed methods include: it provides optimal attitudes even for coplanar baseline configurations; it guarantees convergence even for poor initial conditions; it is a non-iterative algorithm; and it is computationally efficient. These advantages clearly make the new algorithm well suited to on-board applications. The performance of the new algorithm is tested on a dynamic hardware simulator. Results indicate that the new algorithm accurately estimates the attitude of a moving vehicle, and provides robust attitude estimates even when other methods, such as a linearized least-squares approach, fail due to poor initial starting conditions.
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