Full text: Proceedings of ISP Commission 1 symposium on data acquisition and improvement of image quality and image geometry

EEE ORAN FERNE NE 
  
ie o Ru eS ERREICHEN E EE EE. A 
  
aere E Nh NS re NE A etos od nte DM MI RMS NIE ABRE QUEUE DISTRI UMEN INEO Oeste cie ten 
a = - gus t- 3 chant A OA € A N E ater at 4 " 
Carman is a fellow of the Optical Society of America, a member of the 
Canadian Institute of Surveys, and a member of the Canadian Associates of 
Physicists. 
Carman summarizes his present study as follows: 
Angular vibration of aerial survey cameras is a major factor limiting image 
sharpness, either directly or indirectly. The effect is direct if a shutter 
speed is chosen at which image motion due to vibration significantly reduces 
sharpness. It is indirect if, to avoid blurring due to image motion, a 
high shutter speed is chosen and this high shutter speed necessitates the 
use of a large lens aperture and/or a high speed film, either or both of 
which reduce system resolution. 
Measurements of vibration of modern air survey cameras in a variety of 
aircraft over the last few years have shown maximum angular velocities in 
the range 20 to 50 mr/s (4 to 10 mm/s image velocity at the film). To limit 
image motion due to vibration to 15 um requires shutter speed not slower (9 
than 1/270 to 1/660 s. Two comparisons are informative. 1) Image velocity 
due to forward motion in high altitude photography is typically 1.2 to 2.2 
mm/s. 2) Measurements made thirty years ago on reconnaissance camera 
mounts showed 20 mr/s maximum for a standard mount, and 2.5 mr/s for an ex- 
perimental mount. 
According to Carman: if survey mounts could be developed to consistently 
reduce maximum angular vibration velocities to 5 mr/s or less, vibration would 
cease to be a practical limitation in present conditions and system resolu- 
tions could improve by as much as 407. 
Juhani Hakkarainen received his PHD from the Helsinki University of Technology, 
  
Finland, his dissertation on thesis covering laboratory and correlated 
flight tests of photographic image quality and camera calibration. 
Hakkarainen has conducted research on photogrammetric sensors, testing and 
calibration procedures, and has taught photogrammetry at the Helsinki 
University of Technology. He is now professor of Photogrammetry at the 
Finnish Geodetic INstitute where he will continue his research. (9 
Hakkarainen's plans, in assisting WG-3, will extend his image quality 
studies so that the environmental effects on image properties can be de- 
termined. In order to accomplish this investigation, it is planned that 
the Malmi test field in Finland will be enlarged to accommodate higher 
flight altitudes. Additional targets of different sizes and types as used 
in analytic photogrammetry will also be employed. Lower contrast targets 
will be added to the higher contrast ones of the 1973 tests, contrasts of 
1:3 and 1:10-15 being considered because of their "natural" values. 
Five or more transducers will be installed at different parts of the camera, 
and as the external and ambient environments are monitored, the temperature 
and pressure of the camera will be recorded. 
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