Map display system for vehicle navigation

• US 4,896,154 A
• Filed: 10/28/1987
• Issued: 01/23/1990
• Est. Priority Date: 10/28/1987
• Status: Expired due to Fees

• Current Assignee: Eventide, Inc.
• Original Assignee: Eventide, Inc.
• Inventors: Factor, Richard C., Strowe, John A., Pearsall, Terry L., Nass, Laura A.
• Primary Examiner(s): Orsino, Joseph A.
• Assistant Examiner(s): SWARTHOUT, BRENT
• Application Number:
  US07/114,300
• Time in Patent Office: 818 Days
• Field of Search: 340/995, 340/988, 340/990, 340/972, 364/449, 364/443, 364/428, 364/452, 364/460, 73/178 R
• US Class Current: 340/995.27
• CPC Class Codes: G01C 23/00 Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
• CPC Class Codes: G05D 1/0653 during a phase of take-off or landing
• CPC Class Codes: G09B 29/106 using electronic means

Abstract

A map display system includes a vehicle symbol positioned in relation to background map data, and provides a large amount of relevant, easy-to-read map data to a user in a brief period of time. A first feature of the invention involves the drawing of aircraft landing and take-off areas in true size and orientation relative to background map data. A second feature involves display of navigation control areas in relation to an aircraft symbol. In accordance with a third feature, a user can select for display only objects meeting preselected criteria, such as airports having runways of a minimum length. A user can select an object for which text appears on the screen adjacent to that object and which may indicate relative position or distance to such object from the vehicle, in accordance with a fourth feature. A user can select full screen text of information concerning an object on a screen display, in accordance with a fifth feature. A sixth feature provides an automatic alert for an increased oncoming minimum safe altitude for aircraft flight. In an seventh feature, background map data is held stationary while a vehicle symbol moves in relation to the background map data. An emergency aircraft mode of operation, in accordance with an eighth feature, causes automatic display of at least a predetermined number of suitable landing sites according to preselected criteria, such as minimum runway length. A ninth feature involves display of planned and actual travel patterns of a vehicle.

Claims

1. Map display system for navigation of a vehicle showing selected map features in true size and orientation in relation to background map data, the system comprising:

memory means to store map data of an area in which the vehicle may travel;

such data including background map data in a first memory location;

reference location points of selected map features in a second memory location, and true size and orientation data of such selected map features in a third memory location;

first means to selectively collect background map data from the memory means and to compose a first image component of such data;

second means to selectively collect from the memory means reference location points of one or more individual features from the selected map features and true size and orientation data of the one or more selected features within the range of the first image component and to compose a second image component of the one or more selected map features aligned with and in true size proportion to the first image component; and

display means to collectively display the first and second image components.

2. The map display system of claim 1, wherein the vehicle comprises an aircraft and the selected map features comprise aircraft landing and take-off areas.

3. The map display system of claim 2, further comprising:

third means to compose a third image component of a symbol for the aircraft;

means to receive position and direction of travel data for the aircraft and to determine placement of the third image component relative to the first and second image components; and

means included in the display means to display the third image component along with the first and second image components.

4. The map display system of claim 2, wherein the landing and take-off areas comprise runways, the memory means comprises means to store identifiers of runway ends, and the second means includes means to collect data of such identifiers and to include the same in the second image component.

5. The map display system of claim 3, wherein the first and second means include respective means to repeatedly recompose the first and second image components to show movement of such image components, and the third means includes means to maintain the third image component in static position.

6. The map display system of claim 3, wherein the first and second means include respective means to hold the first and second image components in static position, and the third means includes means to repeatedly recompose the third image component to show movement of the aircraft symbol.