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IGI's AEROcontrol system is used to precisely determine
the position and attitude of an airborne camera or other sensor at a given
instant. This can be the position of the projection center and the
omega, phi, kappa angles of the sensor.
Depending on GPS
constellation and distance from GPS Base/Monitor Station, a
positioning accuracy better than 0.1m RMS and attitude accuracy of
0.01 deg RMS is available in post-processing.
The AEROcontrol
system consists of a fiberoptic gyro based Inertial Measurement Unit
(IMU-Ild), a 12-channel L1/L2 Survey GPS receiver, and an airborne
computer. The IMU is mounted rigidly to the sensor system.
The AEROcontrol
system is controlled via the airborne computer or via IGI's Standard
CCNS-4 guidance, positioning and management system for aerial survey
flight missions. AEROcontrol with IGI's fibre-optic based IMU plus Standard CCNS4
form the only fully integrated guidance, management, precise positioning and
attitude determination system available. The system may be installed as separate
units or in a single 19" rack mount, 3U or 5U high.
The airborne computer of the AEROcontrol
system is used for data recording of
- IMU-IId raw
angular and acceleration data at 64 Hz (128 Hz
optional);
- GPS raw data,
positions and velocities;
- Optionally, attitude information from Somag
GSM-3000, Zeiss T-AS, or Leica PAV30 stabilized mount.
All accumulated
raw data are stored on
the AEROcontrol MISSION CARD for post flight processing using the AEROoffice software suite. The system
records approximately 12MB (64Hz) or 18MB (128Hz) of data per hour,
giving essentially unlimited mission time with gigabyte PC-Cards. The processed data can be used as is, or
introduced as additional observations into aerial triangulation /
block adjustment programs (e.g. MATCH-AT or BINGO).
Real-time
platform calculations allow this information to be used as navigational
input for IGI's Standard CCNS4.
When AEROcontrol is used with a sensor
mounted on the GSM-3000, the
highly-accurate gyros of the inertial platform can be used to control stabilization for
better leveling and angular control.
Installation kits for the inertial
measurement unit (IMU) of the AEROcontrol system, including
adapter plate where needed, are available for Wild/Leica RC10A and RC20/RC30,
Zeiss Jena LMK, LMK-1000, and LMK2000, and Zeiss Oberkochen RMK-TOP aerial cameras, and for
Vexcel UltraCam-D and other digital cameras and sensors.

AEROcontrol airborne system:
- Inertial
measurement unit (IMU-11d) with fibre-optic gyros (FOG)
- Integrated
Z-Xtreme/IGI, 12-channel L1/L2 Survey GPS receiver (Ashtech),
modified for airborne operations
- Airborne
AEROcontrol computer Operation a-f vd management of the
AEROcontrol system is either:
- as a stand-alone
system - or controlled by the Standard CCNS4 as an integrated
system
DGPS system:
- Portable GPS
Base / Monitor station, e.g. from IGI (based on Ashtech Z-Xtreme)
with 12 hours or more continous operating time (battery
based)
- Information from fixed
GPS network, e.g. SAPOS in Germany, UK FIXED GPS NETWORK
AEROoffice software package:
- DGPS
computations by GrafNav software package (licence included, others
on request)
- Kalmann
filter software for combined GPS / IMU calculation
- Lever-arm
correction
- Boresight
transformation
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