Ground collision avoidance system

• US 5,136,512 A
• Filed: 02/22/1991
• Issued: 08/04/1992
• Est. Priority Date: 06/26/1988
• Status: Expired due to Term

• Current Assignee: Cubic Defense Systems, Inc. (Cubic Corporation)
• Original Assignee: Cubic Defense Systems, Inc. (Cubic Corporation)
• Inventors: Le Borne, Richard C.
• Primary Examiner(s): Black, Thomas G.
• Application Number:
  US07/659,521
• Time in Patent Office: 529 Days
• Field of Search: 364/461, 364/433, 364/427, 340/970, 340/963, 342/165
• US Class Current: 701/301
• CPC Class Codes: G01C 5/005 altimeters for aircraft G01C5/02, G01C5/06 take precedence
• CPC Class Codes: G05D 1/0083 to help an aircraft pilot in the rolling phase

Abstract

A method and system for avoiding ground collision through pilot warning messages which is implemented in aircraft having a plurality of sensors, onboard inertial navigation units, and altimeters for measuring aircraft performance or flight characteristics. Data is collected through a digital interface unit from data buses connected to these sources, transferred to one or more storage locations and a data validation unit for determining the validity of current altitude data. A series of data processing elements use the aircraft data to extrapolate an aircraft altitude path forward during a predetermined period of time as a function of the aircraft flight data. The extrapolated altitutde allows extrapolation of an aircraft flight path as a function of predicted terrain variations and changes in altitude in response to recovery from various aircraft maneuvers such as rolling, banking, diving, climbing, or accelerating. The extrapolated altitude, or changes in altitude, is compared to one or more predetermined safety limits, and one or more warning messages are provided if the extrapolated altitude is lower than an appropriate limit.

Claims

1. In an aircraft navigation system including a plurality of navigation sensors for producing navigation data and an aircraft data bus connected to said navigation sensors for conducting said navigation data, an apparatus for warning aircraft pilots of potential collisions with terrain comprising:

process control means for controlling the transfer and storage of data in said warning apparatus and for initiating processing steps;

digital interface means connected between said aircraft data bus and said process control means for interfacing said aircraft data bus for transferring data therebetween;

shared storage means connected to said process control means for accumulating navigation data detected on said bus;

data validation means connected to said process control means for detecting the validity of altitude data;

data processing means connected to said process control means for extrapolating a terrain rate estimate in response to said altitude data, for extrapolating a dive/climb angle in response to said terrain rate estimate, for producing a dive recovery time in response to said extrapolated dive/climb angle, for producing a pilot response time, for producing a roll recovery time, and for producing altitude loss data in response to said pilot response time, said roll recovery time, and said dive recovery time; and

warning means connected to said process control means for providing warnings based on an output of said data processing means.

2. The warning system of claim 1 wherein said digital interface means comprises:

at least one remote terminal connected to said aircraft data bus; and

interface process control means connected between said remote terminal and said process control means for polling said remote terminal for collected data, for formatting said data into a collected data message, and for transferring said collected data message to said process control means.

3. The warning system of claim 1 wherein said warning means comprises:

a storage means for storing a series of preconfigured messages corresponding to predetermined altitude and flight path criteria; and

selection means connected to said storage means and to said data processing means for retrieving a message; and

output means for configuring said retrieved message as an aural message.

4. The warning system of claim 3 wherein said warning means comprises second output means for configuring said retrieved message as a visual display.