Pulse radar altimeters

• US 4,241,346 A
• Filed: 07/11/1979
• Issued: 12/23/1980
• Est. Priority Date: 07/11/1979
• Status: Expired due to Term

• Current Assignee: The secretary of state for defence in her Britannic Majesty's Government of the United Kingdom of Great Britain And Northern Ireland
• Original Assignee: The secretary of state for defence in her Britannic Majesty's Government of the United Kingdom of Great Britain And Northern Ireland
• Inventors: Watson, George C.
• Primary Examiner(s): Hubler, Malcolm F.
• Application Number:
  US06/056,678
• Time in Patent Office: 531 Days
• Field of Search: 343/7.5, 343/5 SW, 343/7 A, 244/160
• US Class Current: 342/74
• CPC Class Codes: G01S 13/106 using transmission of pulses having some particular characteristics G01S13/12, G01S13/22, G01S13/24, G01S13/26, G01S13/28 and G01S13/30 take precedence

Abstract

The invention relates to pulse radar altimeters for aircraft wherein the altimeter includes a variable beam width receiver antenna for receiving radar ground echoes, a timer for measuring time intervals between transmitted pulses and received ground echoes thereof, and control means responsive to the output of the timer and arranged to vary the beam width of the antenna in accordance with the values of the measured time intervals.

Claims

1. An aircraft radar altimeter comprising,

a transmitter for transmitting radar pulses,

a variable beam width antenna for radiating the output of the transmitter towards the ground,

a receiver for receiving radar ground echoes,

a timer connected to receive inputs from said transmitter and receiver for measuring time intervals between the transmission of each said pulse and the reception of a corresponding ground echo signal the intervals being proportional to search altitude of said aircraft,

and control means responsive to output of said timer and arranged to vary the beam width of the antenna in accordance with the values of the measured time intervals.

2. An aircraft radar altimeter as in claim 1 wherein said control means is arranged to vary the beam width of the antenna between a low and a high value whenever said timer output reaches a predetermined value, the low value of beam width corresponding to a timer output below said predetermined value.

3. A pulse radar altimeter as in claim 1 or claim 2 wherein said transmitter antenna is a diode controlled multi-slot array antenna.

4. An aircraft radar altimeter comprising,

a transmitter for transmitting radar pulses,

a variable beam width transmitter antenna for radiating the output of the transmitter towards the ground,

a variable beam width receiver antenna for receiving radar ground echoes,

a receiver connected to receive signals from said receiver antenna,

a timer connected to receive inputs from said transmitter and receiver for measuring time intervals between the transmission of each said pulse and the reception of a corresponding ground echo signal, the intervals being proportional to search altitude of said aircraft,

and control means responsive to output of said timer and arranged to simultaneously vary the beam widths of the antennas in accordance with the values of the measured time intervals.

5. An aircraft radar altimeter as in claim 4 wherein the control means is arranged to vary the beam widths of both antennas between a low and a high value whenever said timer output reaches a predetermined value, the low value of beam widths corresponding to a timer output below said predetermined value.

6. A pulse radar altimeter as in claim 4 or claim 5 wherein both said antennas are diode controlled multi-slot array antennas.