Abstract
In this paper, a novel technique for finding a point-by-point (deterministic) attitude solution of a vehicle using Global Positioning System phase difference measurements is presented. This technique transforms a general cost function into a more numerically efficient form by determining threedimensional vectors in either the body or reference coordinate system. Covariance relationships for the new algorithm, as well as methods which minimize the general cost function, are also derived. The equivalence of the general cost function and transformed cost function is shown for the case of orthogonal baselines or sightlines. Simulation results are shown which demonstrate the usefulness of the new algorithm and covariance expressions.
| Original language | English |
|---|---|
| Pages | 23-31 |
| Number of pages | 9 |
| State | Published - 1997 |
| Event | Guidance, Navigation, and Control Conference, 1997 - New Orleans, United States Duration: Aug 11 1997 → Aug 13 1997 |
Conference
| Conference | Guidance, Navigation, and Control Conference, 1997 |
|---|---|
| Country/Territory | United States |
| City | New Orleans |
| Period | 08/11/97 → 08/13/97 |
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