Parameswaran, V and Umesh, BN (2001) Attitude Determination of Aircraft Using GPS Signals. Technical Report. National Aerospace Laboratories, Bangalore, India.
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Abstract
This report details the development of various algorithms in MATLAB / C language for the attitude determination of aircraft using differential GPS phase measurements. The validation of the algorithms is carried out using simulated data. Robustness studies of the algorithms is under progress.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Unit vector13; Attitude;Differential GPS;Direct phase measurements;Baseline length;Unit vector |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance AERONAUTICS > Aircraft Communication & Navigation |
| Division/Department: | Flight Mechanics and Control Division, Flight Mechanics and Control Division |
| Depositing User: | Mrs Neetu Chandra |
| Date Deposited: | 13 Jun 2006 |
| Last Modified: | 24 May 2010 09:42 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1520 |
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