Combined radar/barometric altimeter

• US 4,431,994 A
• Filed: 05/06/1981
• Issued: 02/14/1984
• Est. Priority Date: 05/06/1981
• Status: Expired due to Fees

• Current Assignee: The United States of America As Represented By The Secretary of Agriculture
• Original Assignee: United States Of America As Represented By The Secretary Of The Air Force
• Inventors: Gemin, Robert A.
• Primary Examiner(s): Cangialosi, Sal
• Assistant Examiner(s): Kaiser, K. R.
• Application Number:
  US06/260,879
• Time in Patent Office: 1,014 Days
• Field of Search: 340/27 AT, 340/27 NA, 340/815.02, 340/27 R, 343/12 A, 343/50 P, 343/7 ED, 343/5 R, 343/112 A, 343/7 TA, 364/433, 364/562, 73/178 T, 73/178 R
• US Class Current: 342/120
• CPC Class Codes: G01C 5/06 by using barometric means
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/935 for terrain-avoidance

Abstract

An altitude sensing arrangement which combines the advantages of a barometric altimeter with a radar altimeter. The apparatus monitors the radar altimeter'"'"'s associated radar validity signal and selects the radar altimeter'"'"'s reading when the validity signal indicates a valid condition. Alternately, when the validity signal does not indicate a valid condition, the invention computes the difference in barometric altitude since the last valid radar altimeter reading and sums this difference with the last valid reading from the radar altimeter to produce a combined altitude reading.

Claims

1. A method for supplying altitude signals to an output bus using radar and barometric altimeters, comprising the steps of:

a. selecting the altitude signals from the radar altimeter for output to the output bus if a validity indicator shows them to be valid;

b. computing the change of altitude from the barometric altimeter over a given unit of time;

c. adding said change to the altitude signals on said output bus to provide corrected altitude signals; and

d. if the radar altitude signals are not valid, alternatively selecting said corrected altitude signals for output to the output bus;

the valid or not valid status of the radar altititude signals being used as the sole criteria whether to select the altitude signals from the radar altimeter or the corrected altitude signals.

2. Apparatus for determining the altitude of an aircraft with respect to the underlying terrain, for use with a radar altimeter having an associated validity signal output, and a barometric altimeter, and providing output data for an altitude indicator, said apparatus comprising:

a radar input memory coupled to the radar altimeter, a barometric input memory coupled to the barometric altimeter, a validity bistable device coupled to said validity signal output, timing means which produces timing signals in cycles recurring at fixed intervals;

the timing means having connections with signals effective during each cycle to load radar altitude in the radar input memory, the validity signal condition in the validity bistable device, and barometric altitude data in the barometric input memory;

an output memory having an output to an output bus which is coupled to supply said output data to said altitude indicator, a control input from the timing means to the output memory;

data select means having a control input from the validity bistable device, data input means from the radar input memory, and data output means coupled to the output memory, the data select means being enabled during every cycle in which the state of the validity bistable device indicates that the radar altitude data is valid to cause altitude data to be transferred from the radar input memory to the output memory, so that when the radar altitude data is valid the output data on the output bus represents solely the radar altimeter output;

a second barometric memory having input connection means from the barometric input memory and the timing means enabled during each cycle before current cycle data is loaded into the barometric input memory to transfer the preceeding cycle data from the barometric input memory to the second barometric memory;

adder means having positive data inputs from the barometric input memory and the output bus, a negative input from the second barometric memory, and a data output to a second data input means of the data select means;

the data select means being alternatively enabled during cycles in which the state of the validity bistable device indicates that the radar altitude data is not valid to cause data to be transferred from the adder means output to the output memory, so that when the radar altitude data is not valid the output data on the output bus represents essentially the last valid radar altimeter output updated by the change of the barometric altimeter output;

the valid or not valid status of the radar altitude signals being the sole criteria during each cycle as to whether to select the altitude signals from the radar altimeter or from the adder means.

3. The apparatus of claim 2, wherein the coupling between the data select means and the output memory includes a buffer memory, with a control connection to the timing means, the buffer memory and output memory being enabled by the timing means during each cycle to load data from the data select means into the buffer memory and subsequently from the buffer memory into the output memory to ensure that the data is stable before loading it into the output memory.

4. The apparatus of claim 3, further including an analog-to-digital converter coupled between the radar altimeter and the radar input memory, a synchronous-to-digital converter coupled between the barometric altimeter and the barometric input memory, the data being handled in the apparatus in digital form;

and

wherein said timing means comprises a master clock driving a ring counter, and delay means, the ring counter providing first, second, third and fourth strobe pulses in sequence, with the first strobe pulse supplied to the analog-to-digital and synchronous-to-digital converters, the second strobe pulse supplied to the radar input memory, to the second barometric memory, and via the delay means to the barometric input memory, the third strobe pulse supplied to the buffer memory, and the fourth strobe pulse applied to the output memory.

5. The apparatus of claim 4, further including a pilot selectable digital switch for providing a desired altitude in digital format, a comparator means having inputs from said digital switch and from said output bus for comparing said inputs and generating an output signal if the output data on the output bus is less than the setting of the digital switch;

a second bistable device having one input connected to the output of the comparator means and a control input from the timing means for generating a low altitude warning signal, the control input being the fourth strobe pulse via second delay means.