Altitude sparse aircraft display

Claim 2

A hazard avoidance system for use by aircraft in flight comprising: an altimeter providing data indicative of the altitude of the aircraft; a direction sensor providing data indicative of the course of the aircraft; a position sensor providing data indicative of the position of the aircraft; a computer system including a processor, a display and a moving map data generator providing data indicative of the topography of the area surrounding the position of the aircraft as detected by said position sensor; said computer system determining a hazard zone at least in a sector forward of said aircraft and including the projected course of the aircraft and extending vertically a predetermined distance above and below the altitude of said aircraft; said computer system generating from said moving map display data (i) a display of hazards within said hazard zone in a first emphasized display mode and (ii) a display of features of topography beneath said hazard zone underlying or proximate to the projected course of said aircraft in a second de-emphasized display mode contrasting to said first display mode; said computer system detecting when said aircraft arrives at a predetermined distance from a hazard in said hazard zone in or dangerously proximate to the projected course of the aircraft, and changing at least one of said display modes to create a visual change in appearance to attract the attention of an observer.

Claim 3

A hazard avoidance system according to claim 1 including a speed sensor providing data indicative of the speed of the aircraft wherein said computer system (i) determines from the data from said speed sensor and the position of said hazard in said hazard zone a distance from said hazard at which hazard avoidance action by the aircraft is desirable, and (ii) when said aircraft reaches said distance from said hazard further changes the appearance of at least one of said display modes to indicate that hazard avoidance action is desirable.

Claim 4

A hazard avoidance system according to claim 2 wherein said computer system also determines a course of action which would avoid said hazard and communicates said course of action.

Claim 5

A hazard avoidance system according to claim 3 wherein said communication is audible.

Claim 6

A hazard avoidance system according to claim 2 wherein said computer system determines whether any action has been taken and whether such action would avoid the hazard and, if not, communicates an audible warning to undo the action.

Claim 7

A hazard avoidance apparatus for use in an aircraft having an altimeter providing data indicative of the altitude of the aircraft, a direction sensor providing data indicative of the course of the aircraft, and a position sensor providing data indicative of the position of the aircraft when said aircraft is in flight; said apparatus comprising: a computer system including a processor and a display and a moving map data generator providing data indicative of the topography of the area surrounding the position of the aircraft as detected by said position sensor; said computer system determining a hazard zone at least in a sector forward of said aircraft and including its projected course and extending vertically a predetermined distance above and below the altitude of said aircraft; said computer system generating from said moving map display data (i) a display of hazards within said hazard zone in a first emphasized display mode and (ii) a display of features of topography beneath said hazard zone in a second de-emphasized display mode contrasting to said first display mode; said computer system detecting when said aircraft arrives at a predetermined distance from a hazard in said hazard zone which is in or dangerously proximate to the projected course of the aircraft and changing at least one of said display modes to create a visual change in appearance to attract the attention of an observer.

Claim 8

A hazard avoidance apparatus for use in an aircraft having an altimeter providing data indicative of the altitude of the aircraft, a direction sensor providing data indicative of the course of the aircraft, and a position sensor providing data indicative of the position of the aircraft when said aircraft is in flight; said apparatus comprising: a computer system including a processor and a display and a moving map data generator providing data indicative of the topography of the area surrounding the position of the aircraft as detected by said position sensor; said computer system determining a hazard zone at least in a sector forward of said aircraft and including its projected course and extending vertically a predetermined distance above and below the altitude of said aircraft; said computer system generating from said moving map display data (i) a display of hazards within said hazard zone in a first emphasized display mode and (ii) a display of features of topography beneath said hazard zone in a second de-emphasized display mode contrasting to said first display mode; said computer system detecting when said aircraft arrives at a predetermined distance from a hazard in said hazard zone which is in or dangerously proximate to the projected course of the aircraft and changing at least one of said display modes to create a visual change in appearance to attract the attention of an observer.

Claim 9

A hazard avoidance apparatus according to claim 6 wherein said apparatus includes a port for receiving speed sensor data indicative of the speed of the aircraft and wherein said computer system (i) determines from said speed sensor data and the position of said hazard in said hazard zone a distance from said hazard at which hazard avoidance action by the aircraft is desirable, and (ii) when said aircraft reaches said distance from said hazard further changes the appearance of at least one of said display modes to indicate that hazard avoidance action is desirable.

Claim 10

A hazard avoidance apparatus according to claim 6 wherein said computer system also determines a course of action which would avoid said hazard and communicates said course of action.

Claim 11

A hazard avoidance apparatus according to claim 8 wherein said communication is audible.

Claim 12

A hazard avoidance apparatus according to claim 6 wherein said computer system determines whether any action has been taken and whether such action would avoid the hazard and, if not, communicates an audible warning to undo the action.

Claim 15

A method according to claim 11 including the steps of: providing an element for performing the step of determining a distance from said hazard at which hazard avoidance action by the aircraft is desirable; providing an element for performing the step of determining when said aircraft reaches said distance from said hazard, and providing an element for performing the step of further changing the appearance of at least one of said display modes to indicate that hazard avoidance action is desirable.

Claim 16

A method according to claim 12 including the steps of: providing an element for performing the step of determining a course of action which would avoid said hazard, and providing an element for performing the step of communicating said course of action.

Claim 17

A method according to claim 13 including the step of providing an element for performing the step of audibly communicating said course of action.

Claim 18

A method according to claim 12 including the steps of: providing an element for performing the step of determining whether any action has been taken and whether such action would avoid the hazard, and if the action taken would not avoid the hazard communicating an audible warning to undo the action.

Claim 19

A computer program product for implementing hazard avoidance by an aircraft in flight comprising: a computer readable memory medium; and a computer program stored in said memory medium including instructions for converting representations of aircraft in flight speed, course, altitude and plus and inus differentials in altitude into a simulation of a hazard zone surrounding a projected flight path along said course bounded by vertically spaced surfaces spaced by the sum of said differentials; instructions for converting digital representations of a topographical map of terrain subtended by said hazard zone into a first display of hazards rising from said terrain into said hazard zone, and a second display of the terrain subtending said hazard zone but not rising into said hazard zone, and presenting said displays in contrasting styles to enhance said first display relative to said second display; instructions for providing a position determining function relating the position of said aircraft to said first and second displays; instructions for performing a calculation function determining a minimum distance from a hazard in or proximate to said flight path at which evasive action must be undertaken to avoid said hazard, and generating a signal when the position of said aircraft arrives at said distance; and instructions for activating an alarm responsive to said signal, said alarm comprising at least in part a change in the relationship of said first and second displays to one another.

Claim 20

A computer program product for implementing hazard avoidance by an aircraft in flight comprising: a computer readable memory medium; and a computer program stored in said memory medium including instructions for converting representations of aircraft in flight speed, course, altitude and plus and inus differentials in altitude into a simulation of a hazard zone surrounding a projected flight path along said course bounded by vertically spaced surfaces spaced by the sum of said differentials; instructions for converting digital representations of a topographical map of terrain subtended by said hazard zone into a first display of hazards rising from said terrain into said hazard zone, and a second display of the terrain subtending said hazard zone but not rising into said hazard zone, and presenting said displays in contrasting styles to enhance said first display relative to said second display; instructions for providing a position determining function relating the position of said aircraft to said first and second displays; instructions for performing a calculation function determining a minimum distance from a hazard in or proximate to said flight path at which evasive action must be undertaken to avoid said hazard, and generating a signal when the position of said aircraft arrives at said distance; and instructions for activating an alarm responsive to said signal, said alarm comprising at least in part a change in the relationship of said first and second displays to one another.

Claim 21

A computer program product according to claim 16 wherein said alarm comprises at least in part an audible signal.