Expanded field of view (EFOV) display for real-time, manned, interactive air combat simulation, including close-in combat

• US 5,272,652 A
• Filed: 11/01/1991
• Issued: 12/21/1993
• Est. Priority Date: 11/01/1991
• Status: Expired due to Term

• Current Assignee: Eidetics International, Inc.
• Original Assignee: Eidetics International, Inc.
• Inventors: Ettinger, Robert C., Lynch, Urban H. D., Skow, Andrew M., Rosenshein, Leon, Cobasko, James R., Mosher, Steven M., Farmer, Donald I.
• Primary Examiner(s): Harvey, Jack B.
• Assistant Examiner(s): BUROKER, BRIAN
• Application Number:
  US07/786,736
• Time in Patent Office: 781 Days
• Field of Search: 364/578, 364/516, 472/130, 273/434, 273/442, 434/30, 434/37, 434/38, 434/43, 434/19, 358/104, 358/183, 395/119, 395/152, 395/157
• US Class Current: 703/8
• CPC Class Codes: G09B 9/003 for military purposes and tactics
• CPC Class Codes: G09B 9/30 Simulation of view from aircraft

Abstract

An expanded field of view visual display concept capable of conducting credible close-in or within visual range (WVR) air-to-air combat from a single computer graphics display screen. By use of the invention, the visual scene content that normally exists outside and around the cockpit of a fighter aircraft can be condensed onto a single CRT screen or video projection screen in such a manner that pilots have good situational awareness, even in close-in-combat, and can fly credible air combat. An expanded field of view visual display is created, referred to as target coordinate display (TCD), capable of conducting credible close-in simulated air combat from a single CRT display or video projection screen. The display handles multiple aircraft, shows friendly aircraft formations, is usable in real time, shows weapon release information, is easily adapted to by pilots, and yields credible air combat simulation results.

Claims

1. A flight simulator system in which a simulator pilot'"'"'s ownship having a nose and a tail, and target aircraft and friendly aircraft, each having a corresponding nose and tail and wingtip positions, are generated in real time on a display screen under control of flight simulator software, said generated display being a nominal 40°

azimuth by 30°

elevation display view centered around a forward fuselage reference line passing through the nose and tail of the ownship, said flight simulator system comprising;

a) means for obtaining positional, directional and velocity information defining the flight of the ownship, said friendly aircraft and said target aircraft;

b) means for performing predetermined calculations representing the flight of the ownship, said friendly aircraft and said target aircraft based upon said positional, directional and velocity information;

c) means for generating a target coordinate display showing said friendly aircraft and said target aircraft, said generating means including;

i) means for determining whether each of said target aircraft and said friendly aircraft are visible to said ownship pilot;

ii) means for determining whether each of said visible target and friendly aircraft are within said nominal 40°

azimuth by 30°

elevation display;

iii) means for calculating screen positions for each of said visible target and friendly aircraft outside said nominal 40°

azimuth by 30°

elevation display based upon a roll angle between each of said visible target and friendly aircraft outside said nominal 40°

azimuth by 30°

elevation display and said ownship;

iv) means for drawing each of said visible target and friendly aircraft outside said nominal 40°

azimuth by 30°

elevation display within a target display window disposed inside said nominal 40°

azimuth by 30°

elevation display using said calculated screen positions;

v) means for drawing each of said visible target and friendly aircraft within said nominal 40°

azimuth by 30°

elevation display at the actual relative location of each said visible target.

2. The flight simulator system defined by claim 1 wherein said screen positions calculating means comprises a program for calculating the position of a predetermined one of said friendly or target aircraft according to a formula:

space="preserve" listing-type="equation">X coordinate=X screen center+screen radius*sin (DRoll)

space="preserve" listing-type="equation">Y coordinate=Y screen center+screen radius×

cos (DRoll)

where DRoll is said roll angle, X screen center is 1/2 screen width in pixels, Y screen center is 1/2 screen height in pixels and screen radius is 0.9 * X screen center.

3. The flight simulator system defined by claim 2 wherein said drawing means using said calculated screen positions comprises means for displaying said predetermined aircraft within the target display window, said X coordinate and said Y coordinate being a center point of said predetermined aircraft within said target display window.

4. The flight simulator system defined by claim 1 wherein said target coordinate display generating means further comprises means for determining whether flight path ribbons are to be displayed and if said flight path ribbons are to be displayed drawing a series of connection polygons whose corners are defined by the positions of the wingtips of said target and friendly aircraft over a predetermined period of time.

5. The flight simulator system defined by claim 4 wherein said predetermined period of time is 10 seconds.

6. The flight simulator system defined by claim 3 further comprising means within the target display window for graphically indicating the position of said predetermined aircraft relative to the nose of the simulator pilot'"'"'s ownship and a position of the pilot'"'"'s ownship relative to the nose of said predetermined aircraft.

7. The flight simulator system defined by claim 6 wherein said indicating means comprises first and second analog bars within said target display window, said first analog bar representing an angle of said predetermined aircraft to the nose of the pilot'"'"'s ownship and said second analog bar representing an angle of the pilot'"'"'s ownship relative to the predetermined aircraft'"'"'s nose wherein a length of said analog bars each respectively represent said angles and a rate of change of the lengths of the first and second bars conveys to the pilot a sense of which of said ownship and said predetermined target aircraft are obtaining a combat advantage and how rapidly said advantage is being obtained.