Information transmission system

• US 4,768,736 A
• Filed: 02/13/1987
• Issued: 09/06/1988
• Est. Priority Date: 02/14/1986
• Status: Expired due to Fees

• Current Assignee: GEC Marconi Limited (Gooding Consumer Electronics Ltd.)
• Original Assignee: US Philips Corporation (Koninklijke Philips N.V.)
• Inventors: Forder, Stuart, Morten, Frank D.
• Primary Examiner(s): Jordan, Charles T.
• Application Number:
  US07/014,515
• Time in Patent Office: 571 Days
• Field of Search: 244/3.13, 244/3.11, 250/200, 250/215
• US Class Current: 244/3.11
• CPC Class Codes: F41G 7/306 for transmitting guidance signals; F41G7/308 takes precedence
• CPC Class Codes: H01L 31/024 Arrangements for cooling, heating, ventilating or temperature compensation for photovoltaic devices H01L31/052
• CPC Class Codes: H01L 31/02966 including ternary compounds, e.g. HgCdTe

Abstract

An information transmission system is provided for a guided missile 1 in which guidance information is transmitted from the missile launch point to the missile along a beam 8 of 10 μm wavelength radiation. The missile has a rearwards facing optical system 9 to collect and focus the radiation onto a cooled cadmium mercury telluride detector. The proportion of cadmium to mercury in the detector is chosen so that just after launch in the early stage of detector cool-down the long wavelength cut-off of the detector just includes the 10 μm radiation, providing an early guidance signal, and so that, as cooling proceeds, the long wavelength cut-off moves to longer wavelengths thereby rapidly enhancing the received signal to compensate for loss of received energy at the missile due to missile range increase.

Claims

1. An information transmission system for sending information along a beam of radiation of a selected wavelength comprising:

a radiation transmitter and a radiation receiver, the information transmission system sending the information from the radiation transmitter to the radiation receiver, the radiation intensity at the radiation receiver falling as a function of time elapsed from a start of information transmission, the radiation receiver including a radiation detector whose detectivity rises as a function of falling detector temperature and cooling means for progressively reducing the detector temperature from the start of transmission, the detector having a peak in detectivity as a function of wavelength, which peak increases in wavelength from less than the selected wavelength up to at least the selected wavelength as the detector temperature falls towards its operating value.

2. An information transmission system as claimed in claim 1, wherein the peak in detectivity at the operating temperature is at a wavelength longer than the selected wavelength.

3. An information transmission system as defined in claim 2, wherein the detector is a cadmium mercury telluride photoconductive detector, and the relative proportions of cadmium and mercury are selected so that the long wavelength cut-off of the detector substantially equals the selected wavelength before cooling.

4. An information transmission system as claimed in claims 1, 2 or 3, wherein the selected wavelength is 10.6 μ

m.

5. An information transmission system as claimed in claims 1, 2 or 3, wherein the receiver recedes from the transmitter as a function of time from the start of transmission, producing the fall in received radiation intensity.

6. An information transmission system as claimed in claim 5 wherein the receiver is mounted in a guided missile, the start of transmission is the launch instant of the missile, and the information transmitted is missile guidance information.