초록 ▼

The method provides for an information presentation (IF1) to be presented on a visual-display screen (5), the information representing at least one vertical plane along a theoretical flight trajectory of the aircraft, and which includes an axis system (8, 9), in which a y-axis (8) is graduated in al

The method provides for an information presentation (IF1) to be presented on a visual-display screen (5), the information representing at least one vertical plane along a theoretical flight trajectory of the aircraft, and which includes an axis system (8, 9), in which a y-axis (8) is graduated in altitude, and an x-axis (9) is graduated in distance from the position of the aircraft, a particular symbol (7) representing the aircraft, which is arranged on the y-axis (8) at a position representative of the altitude of said aircraft, and a first plot (T1) representing a theoretical flight trajectory of said aircraft in the vertical plane. Said information presentation (IF1) further includes at least one second plot (T2) corresponding to a safety altitude, and a third plot (T3) corresponding to a contour of the terrain (10) in the vertical plane.

대표청구항 ▼

The method provides for an information presentation (IF1) to be presented on a visual-display screen (5), the information representing at least one vertical plane along a theoretical flight trajectory of the aircraft, and which includes an axis system (8, 9), in which a y-axis (8) is graduated in al

The method provides for an information presentation (IF1) to be presented on a visual-display screen (5), the information representing at least one vertical plane along a theoretical flight trajectory of the aircraft, and which includes an axis system (8, 9), in which a y-axis (8) is graduated in altitude, and an x-axis (9) is graduated in distance from the position of the aircraft, a particular symbol (7) representing the aircraft, which is arranged on the y-axis (8) at a position representative of the altitude of said aircraft, and a first plot (T1) representing a theoretical flight trajectory of said aircraft in the vertical plane. Said information presentation (IF1) further includes at least one second plot (T2) corresponding to a safety altitude, and a third plot (T3) corresponding to a contour of the terrain (10) in the vertical plane. A remote vehicle identification and disabling system for identifying and controlling a vehicles engine. The system has a limited ranged programmable transceiver unit mounted in a non-civilian vehicle for sending and receiving a signal through an antenna located in the grille. A control and display unit is located in the cab that allows access to an onboard computer for accessing a remote police database. The system also has a civilian vehicle mounted multiple channel transceiver that controls a fail-open valve which is connected to a fuel line of the civilian vehicle to control the amount of fuel supplied to the engine. The civilian vehicle unit transmits an identification signal to the non-civilian unit upon request and if the civilian unit receives the identical identification signal from the non-civilian unit then the valve will be activated. A remote control unit transmitting at a frequency other than the non-civilian unit can be used to activate the valve. The non-civilian unit transmits at a frequency that has higher priority over the remote control deter from any unauthorized activation of the valve.