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: 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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