Efficient and Optimal Attitude Determination Using Recursive Global Positioning System Signal Operations
Author(s) -
John L. Crassidis,
E. Glenn Lightsey,
F. Landis Markley
Publication year - 1999
Publication title -
journal of guidance control and dynamics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 1.573
H-Index - 143
eISSN - 1533-3884
pISSN - 0731-5090
DOI - 10.2514/2.4373
Subject(s) - convergence (economics) , computer science , nonlinear system , kinematics , algorithm , control theory (sociology) , simple (philosophy) , filter (signal processing) , iterative method , mathematical optimization , mathematics , artificial intelligence , computer vision , control (management) , philosophy , physics , epistemology , classical mechanics , quantum mechanics , economics , economic growth
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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