ONS 
sal-time 
ameters 
ications 
airborne 
itial for 
as been 
correct 
can be 
rs With 
ian be 
7 of 0.1- 
curacies 
aluation 
used as 
latching 
y of the 
for the 
imaging 
e direct 
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obvious 
itioning 
tion of 
ed with 
napping 
ew of 
itioning 
n, Vol. 
1ington, 
Aircraft 
Attitude 
3PS-92, 
of the 
igation, 
| Static 
ibiguity 
ry and 
ol. 185; 
  
HARTL P., WEHR A. [1986]: Coordinate 
Transformation Procedures for GPS-Attitude 
Control, Proceedings of the ISPRS Commission 
I Symposium on Progress in Imaging Sensors, 
ESA SP-252, pp.215-226, Stuttgart, Germany, 
1986 
HATCH R. [1990]: Instantaneous Ambiguity 
Resolution, Proceedings of the IAG Symposium 
107 Kinematic Systems in Geodesy, Surveying 
and Remote Sensing, pp. 299-308, Banff, 
Canada, 1990 
KALAFUS R., VAN DIERENDONCK A., PEALER N. 
[1986]: Special Committee 104 
Recommendations for Differential GPS Service, 
Global Positioning System, Papers published in 
Navigation, Vol. III, The Institute of 
Navigation, Washington, 1986 
LACHAPELLE G., CANNON E., ERICKSON C., 
FALKENBERG W. [1992]: High Precision C/A 
Code Technology for Rapid Static DGPS 
Surveys, Proceedings of the 6th International 
Geodetic Symposium on Satellite Positioning, 
Columbus, Ohio, USA, 1992 
SCHADE H. [1992]: Reduction of Systematic 
Errors in GPS-Based Photogrammetry by Fast 
Ambiguity Resolution Techniques, International 
Archives of Photogrammetry and Remote 
Sensing, Vol. XXIX, Part B1, pp. 223-228, 1992 
SCHADE H. , LACHAPELLE G., CANNON E. [1993]: 
An Accuracy Analysis of Airborne Kinematic 
Attitude | Determination with the 
NAVSTAR/Global Positioning System, SPN- 
Zeitschrift für Satellitengestützte Positionierung, 
Navigation und Kommunikation, Vol. 3/93, pp. 
90-95,1993 
189