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currently on hold and we have been requested to re-submit our proposal with a decision
expected in 2004. Finally, CSP has used its time in Europe to develop an EU-based team with
skills and expertise similar to CSP in North America. The intent is to have the EU team play
a similar role as CSP in education, outreach and stimulating market demand for CMS. CSP,
along with TNO (Netherlands research institute), Johannum (Austria research institute), Green
Alliance (UK policy organization) and InternationalEchem (UK consultancy) met in Vienna
in November 2003 and agreed to submit a proposal to the EU for initial funding to establish
such an organization and pilot the CMS model in several EU countries. The proposal will be
written in 2004.
The CMZ series are state-of-the-art color zoom camera units
offering up to 72x zoom (18x optical + 4x digital) and a multitude
of features including automatic/manual focus control, freeze frame,
low-light operation and digital signal processing. The CMZ’s precision
optics allow you to see the more of the picture with it’s wide
48 degree field of view. To the other extreme you can zoom in full
digital telephoto mode to less than one degree.
The lightweight CMZ-01 is designed to install flush into the belly
fuselage area to provide a downward looking view below the aircraft.
Internal and externally installed versions are available. CMZ-
01 cameras can be controlled via RS-485 data bus or by keyline
control.
• High Resolution
• 72x Zoom
18x Optical and 4x Digital
• Automatic Focus
• Freeze Frame
• Digital Signal Processing
• Low Light Operation
Features:
100-1053-01
— CMZ-01-1 (Internal installation)
100-1053-02
— CMZ-01-2 (External installation)
100-1053-03
— CMZ-01-3 (No mounting plate)
• Airbus
• Bombardier
• Gulfstream
Part Numbers Approved installations include:
• Boeing
• Dassault
• Raytheon
CMZ-01-1
CMZ-01-3
CMZ-01-2
Model CMZ-01-1 CMZ-01-2 CMZ-01-3
Part Number 100-1053-01 100-1053-02 100-1053-03
Description
Camera Unit, Zoom,
Internal Mount
Camera Unit, Zoom,
External Mount
Camera Unit, Zoom,
(no mounting plate)
Max. Weight 1.75 lb. (.79 kg)
Dimensions (HWD)
4.7 x 2.5 x 2.5 in.
(119x64x64 mm)
Mounting Plate Dim 6.02x0.150 in.(1522x4mm) 3.752x0.50 in.(952x1mm) (none)
Finish Powder coated, black
Mounting 4x 10-32 fasteners 8x 10-32 fasteners 4x 4-40 fasteners
Window Material Fused Silica
Window Demisting Internal Heater
Power Requirements 12 VDC, 10w max.
Video Output VBS, 1.0 Vp-p at 75 Ω, Negative Sync
Television System NTSC 3.58 Color
Mating Connector MS3126F14-18S
Horizontal Field of View Optical Mode:18x zoom, 2.7º ~ 48º ; Digital Mode: 72x Zoom, 0.68º ~ 48º
Imager 1/4 inch interline transfer CCD
Resolution >470 Horz. TV Lines
Picture Elements: 380K; 768(h) x 494(v)
Sync: Internal
Gamma: γ=0.45
Min. Illumination: 0.2 lux at f1.4
White Balance: Automatic, through-the-window
Electronic Shutter: 1/60-1/10,000 s plus auto-iris
S/N Ratio: >50dB
Features Autofocus, Freeze-Frame, Low-Light "Night" Mode , Digital Signal Processing
Options Electrical Installation Kit / Cables; Structural Installation Kit
Specifications:
Securaplane Technologies, Inc.
Part of the Pacific Scientific Aerospace Group
10831 N. Mavinee Drive, Tucson, Arizona 85737
Tel. (520) 297-0844 • Fax: (520) 498-4924
www.securaplane.com
0408 r06
Typical Lower
Fuselage Installation.
Zoom camera images taken during a flight test over Tucson, Arizona.
Information subect
to change.
Please contact
Securaplane for
current data.
International Civil Aviation Organization CNS/MET SG/6 – IP/13
Sixth Meeting of CNS/MET Sub-Group of APANPIRG
Bangkok, Thailand, 15 – 19 July 2002
Agenda Item 18): Any other business
DEVELOPMENT OF UPLINK/DOWNLINK OF
OPMET INFORMATION IN HONG KONG, CHINA
(Presented by Hong Kong, China)
SUMMARY
This paper presents the development of uplink and downlink of
OPMET information in support of the new CNS/ATM systems in
Hong Kong, China.
1. Introduction
1.1 The development of the meteorological system in support of the new Communication,
Navigation, Surveillance/Air Traffic Management (CNS/ATM) systems in Hong Kong, China, started
in 2000. Over the past two years, trials were conducted on the downlink of meteorological
information from aircraft. Operational uplink of OPMET information to aircraft was also launched in
　
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