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USER 
REQUIREMENTS 
* 
- GEOMETRIC AVAILABLE 
- RADIONMITRIC REMOTE : E 
—- TUZMPORAL 33NSING 
RESOLUTION ECHNOLOG E 
UT T oa REQU 
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GENERAL DEFINITION OP à SPACE 
REMOTE SENSING MISSION €— 
- ORSIT = PLATFORM — SENSOR SI 
coverace attitude type GEC 
altitude drift swath width OF 
COMPUTER SIMULATION 
— ORBITAL -— PLATFORM ~- SENSOR | suv] [Dme| |amwospuEnE] € 
MOTION ATTITUDE SES | | GEOG 
GEOMETRY » AND R/ 
| GEOMETRIC AND DATA FROM OF 
RADIOMETRIC RESULTS OTHER SENSORS 
i fig. | 
|SIMULATED IMAGE M———— — —— 
inves 
USER proce: 
REQUIREMENT Capri 
SATISFIED a sca. 
The a. 
NEW tical 
PARAMETERS : obtai: 
DEFINITION APPLICATION In fi 
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The à 
geoid 
fig. 1 Simulation of a proposed space rerote sensing mission ue 
& 
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information system in order to compare it with data from other : 
Sources, Several images can be analyzed on the same area, giving viewi 
also the possibility of simulating new missions. "ITY 
an al 
and 2 
PRELIMINARY CONSIDERATIONS ON THE SPOT SATELLITE 
; diffe 
The italian SPOT simulation will start practically in frame 
October 1982 when the Daedalus CCTs will be delivered to the acros 
26