The objectives of the Guidance and Control Panel Working Group 04 were to consider the integration of GPS in aircraft systems and make recommendations for implementation. Volume IID addresses the fourth of those specific studies. The availability of the NAVSTAR/GPS opens the way to the use of simpler gyros in a strap-downs system. The influence of GPS aiding of a strap-down system on the accuracy requirements for the gyros is investigated in this paper for RPV mission.
The Impact of Global Positioning System on Guidance and Controls Systems Design of Military Aircraft. Volume IID. Specific Study Number 4: Gyro Accuracy Requirements in a Strap Down Inertial Navigation System with GPS Aiding for RPV Missions
1980
17 pages
Report
No indication
English
Avionics , Navigation & Guidance System Components , Global positioning system , Flight instruments , Inertial navigation , Gyroscopes , Strapped down systems , Accuracy , Military aircraft , Military requirements , Remotely piloted vehicles , Error analysis , Foreign Technology , NATO furnished , NAVSTAR Project
NTIS | 1978
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