DocumentCode :
3448294
Title :
Test flights of GNSS1 at high latitudes
Author :
Richards, G. ; McGregor, A.E. ; Harlow, R.A. ; Watt, A. ; Tiemeyer, B.
Author_Institution :
Defence Res. Agency, Bedford, UK
fYear :
1995
fDate :
35019
Firstpage :
42461
Lastpage :
410
Abstract :
As the first step towards a civilian global navigation satellite system (GNSS) it is proposed to augment the existing GPS system with integrity and ranging signals broadcast by Inmarsat geostationary satellites. This paper presents the results of a flight trial conducted to assess the visibility of these geostationary satellites at the edge of coverage at northern latitudes. The trial was carried out in a DRA BAC 1-11 aircraft in order to assess the use of the satellites for civil airborne navigation. The observed visibility of the geostationary satellites is compared with theoretical simulations, highlighting the reception at the edge of coverage and the effects of the aircraft manoeuvring. The visibility of the geostationary satellites is described with particular emphasis on the approaches and landings. The performance of the GPS system during the trial is also discussed, in terms of accuracy, availability, continuity of service and the ability to provide an integrity capability. Finally, the effects of changing the elevation mask angle and of including the geostationary satellites as ranging sources are examined
Keywords :
Global Positioning System; aircraft testing; BAC 1-11 aircraft; GNSS1; GPS system; Inmarsat geostationary satellites; accuracy; aircraft manoeuvring effects; availability; civil airborne navigation; elevation mask angle; flight trial; geostationary satellites visibility; high latitudes; integrity signals; northern latitudes; observed visibility; ranging signals; ranging sources; reception; service continuity; test flights; theoretical simulations;
fLanguage :
English
Publisher :
iet
Conference_Titel :
Implementation of GNSS, IEE Colloquium on
Conference_Location :
London
Type :
conf
DOI :
10.1049/ic:19951308
Filename :
494807
Link To Document :
بازگشت