Process for displaying flying aid symbols on a screen on board a

Communications: electrical – Aircraft alarm or indicating systems – Nonalarm flight indicator

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73178T, 340972, 340973, 340974, 340975, 364428, 36442406, G01C 2100

Patent

active

052891852

ABSTRACT:
The invention relates to a process for the display on a screen on board an aircraft of flying aid symbols. On the basis of information supplied by an inertial system and ground beacons processed by an on board computer, the process consists of displaying on an on board screen (EV) symbols more particularly representing the wings of the aircraft (A1, A2), the model of the aircraft (CP), its speed (V), the tendency to acceleration and deceleration (AD1, AD2), a flight path prediction (PT), the artificial horizon (H), the roll angle (.phi.), the sideslip (AL) and the total energy (ET1, ET2). It also consists of displaying the flight path to be followed in perspective (P1, P2, S3, S4, S5) and in projection (S'1 to S'5) on the plane of the runway. Any flight path segment during passage, as well as the segment following the latter are displayed in parallelepipedic form (P1, P2) in perspective. A final segment preceding the touchdown point of the wheels on the runway is displayed in the form of a pyramid (P3) in perspective. A display also takes place of the runway (P) and a grid (M1, M2, PE1, PE2) superimposed on said runway, in perspective.

REFERENCES:
patent: 3784969 (1974-01-01), Wilckens et al.
patent: 4121246 (1978-10-01), Fadden et al.
patent: 4368517 (1983-01-01), Lovering
patent: 4419079 (1983-12-01), Georges et al.
patent: 4825194 (1989-04-01), Rasinski
patent: 4999780 (1991-03-01), Mitchell
patent: 5025382 (1991-06-01), Artz
Proceedings of the 1988 IEEE International Conference on Systems, Man and Cybernetics Aug. 8-12, 1988, vol. 1, pp. 506-508, Christopher Wickens et al.

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