Attitude Determination of Aircraft Using GPS Signals

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: Monograph (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
Depositing User: Users 49 not found.
Date Deposited: 13 Jun 2006
Last Modified: 24 May 2010 04:12
URI: http://nal-ir.nal.res.in/id/eprint/1520

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