leica pav100 · pav100 heavy load 65 kg to 100 kg typical residual deviation from vertical* <...
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Leica PAV100 Gyro-stabilised Sensor Mount
The Leica PAV100 Gyro-stabilised Sensor Mount
provides angular motion compensation, perfectly
vertical photography and automatic drift control for a
wide range of airborne sensors.
Precise sensor stabilisation during camera exposure is
essential for good image quality. The new Leica
PAV100 keeps the camera in stable nadir view and fully
compensates for any aircraft movement during the
active exposure time. It provides automatic drift control
and pitch, roll compensation using precise IMU data.
Introducing an unique Adaptive Control feature which
filters out environmental vibrations.
The stabilised mount is compatible with Leica and Z/I
Imaging airborne sensors as well as a wide range of
other sensors, allowing the user to change quickly
between sensors inside a unified aircraft installation.
This reduces cost and simplifies operation.
Leica PAV100 Key Benefits
Cost savings nMore efficient photo flights
n Less stress on the flight crew
n Fewer flight lines due to perfect drift compensation
and accurate side lap
Best Stabilisation n Automatic correction for angular motion
n Perfect vertical photography
n Superior image quality
n Automatic drift setting
nWide stabilisation range
Any System n Leica ADS80 and Leica ADS100
n Leica RCD30 Standalone and Leica RCD30 Oblique
n Leica ALS60 and Leica ALS70
n Z/I DMC IIe digital frame camera series
n AHAB DragonEye, Chiroptera II, HawEye III
n Support 3rd party interface for any airborne sensor
Any Flight Condition n Fast, wide-range angular motion compensation
as required during turbulent flights
nHigh-accuracy stabilisation to stabilise during smooth flights
nOperates in a wide environmental range
Leica PAV100 Features n Adaptive Control to filter out environmen-
tal vibrations to reduce the angular rate
residual by a factor of 2.
n Angular motion compensation
n Automatic perfectly vertical photography
n Fully automated operation
n Automatic drift setting
n Automatic initialisation and system test
during startup
n Remotely controlled operation via Leica
FlightPro (Flight guidance & Sensor
Control Management System) or com-
mand interface to 3rd party FMS
n PAV100 Control Software for simple initial
setup and diagnosis
nOutputs gimbal data at high data rates
n Reliable, high-quality hardware conform-
ing to ISO 7137, RTCA DO-160G, EURO-
CAE-14G, FAR§23.561 and FAR§27.561
nDirect interchange with Leica PAV30 and
Leica PAV80 installations
n Fully integrated in the Leica Geosystems
Airborne Sensor workflow, including
Novatel SPAN operation
n Proven gimbal suspension design with
high torque motors
n Flexible mechanical interfaces support
various sensor types
n Adaptable to sensor weight from 5 kg up
to 100 kg without the need for mass compensators n Interfaces to 3rd party GNSS/IMU Systems
n Interface to SPAN-IGM GNSS/INS System
to support PAV100 standalone operation
Leica PAV100 Gyro-stabilised Sensor Mount
Leica PAV100 Product Specifications standard low height
Operational Stabilisation range in roll – 7° to + 7° – 5° to + 5°
Stabilisation range in pitch – 8° to + 6° – 5° to + 5°
Stabilisation range in drift – 30° to + 30°
Sensor weightPAV100 5 kg to 75 kg
PAV100 heavy load 65 kg to 100 kg
Typical residual deviation from vertical* < 0.02° RMS
Typical residual deviation from drift* < 0.02° RMS, depends on GNSS/IMU
Interfaces Command interface RS232
GNSS/IMU System RS232 to Leica IPAS20, Novatel SPAN or 3rd
party GNSS/IMU system
Electrical Voltage input 22.0 to 30.3 VDC
Power Consumption at 28 VDC Average ** 35 W, Peak 250 W
Pre-fuse rating Min 10 A, Max 15 A
Mechanical Mechanical sensor interfacesSH81, SH82, SH91, SH92, SH100, RCD30
DMCIIe, ALS60/70 with RCD30, Generic
Sensor hole dimension 410 mm
Dimension PAV100 673 mm x 532 mm x 168 mm
Weight excluding sensor adapters 38.0 kg
Environmental Operating Temperature – 20 °C to + 55 °C
Storage Temperature – 40 °C to + 85 °C
Pressurised aircraft / non pressurised ICAO 50,000 ft / ICAO 25,000 ft
Humidity 0 % to 95 % rH according to ISO 7137
Applied Standards General ISO 7137, RTCA DO-160-G, EUROCAE-14G
Emergency Landing FAR§23.561, FAR§27.561
Conformity to National Regulations CE, FCC Part 15
* For photo flight situations, i.e. aircraft angular motion < 10 °/s and with typical aircraft photo flight frequency spectrum** For balanced weight
Illustrations, descriptions and technical data are not binding. All rights reserved. Printed in Switzerland – Copyright Leica Geosystems AG, Heerbrugg, Switzerland, 2014. 808522en – 07.14 – galledia
Leica Geosystems AG Heerbrugg, Switzerland
www.leica-geosystems.comhttp://di.leica-geosystems.com
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