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Gulfstream HUD Pilot's Control Unit

Technical Information

Catalogue No: C0339
Category: Head-Up Display [HUD]
Object Type: Control/Data Entry
Object Name: Gulfstream HUD Pilot's Control Unit
Part No: 92-056-01
Serial No: G001
Manufacturer: GEC Avionics
Division: Unknown
Platform(s): Gulfstream IV 
Year of Manufacture:
Dimensions:
Width (mm):
145 
Height (mm):
140 
Depth (mm):
140 
Weight (g):
1,580 
Location: Main Object Store
Inscription(s):

92-056-01
Ser No G001

Notes:

In the early 1990s the US Federal Aviation Administration (FAA) began a flight test programme of a synthetic vision system (SVS) to gather data for that certification. The SVS was a joint programme with the US Defence Department to develop technology enabling low visibility landings on what they called "cooperative" and "non-co-operative" runways. Their Gulfstream II test bed was equipped with a HUD and both IR and MMW, to balance the advantages and disadvantages of the two sensors. The pilot was able to switch between the two sensors initially, but there were plans to blend the images later.

GEC Avionics supplied an overhead HUD system made from F-16 and C-17 components and a separate electronics unit located in the avionics bay. Kodak supplied the mid-wave IR and Honeywell and Lear two different MMW radars.

The Electronics Unit is from this Gulfstream II "Synthetic Vision Experimental Program". It later went on to be fitted to a BAC 1-11 research aircraft by Westinghouse in Baltimore to support their Boeing supported "ESAS" program in concert with Honeywell, and eventually led to the Honeywell connection with Marconi Avionics.

This is the HUD Control Panel for the Gulfstream II system.

Click to enlarge