초록 ▼

Methods and systems for operating an avionics system on-board an aircraft are provided. In one embodiment, data associated with a take off roll is received, one or more v-speeds of the aircraft associated with the take off roll are calculated, and during the take off roll, the aircraft is controlled

Methods and systems for operating an avionics system on-board an aircraft are provided. In one embodiment, data associated with a take off roll is received, one or more v-speeds of the aircraft associated with the take off roll are calculated, and during the take off roll, the aircraft is controlled based on the one or more calculated v-speeds.

대표청구항 ▼

1. A method for controlling an aircraft during an automated take off, the method comprising: receiving realtime data associated with the aircraft during a take off roll;calculating, by a processor, one or more v-speeds of the aircraft associated with the take off roll based on the realtime data; and

1. A method for controlling an aircraft during an automated take off, the method comprising: receiving realtime data associated with the aircraft during a take off roll;calculating, by a processor, one or more v-speeds of the aircraft associated with the take off roll based on the realtime data; andduring the take off roll, controlling the aircraft based on the one or more calculated v-speeds. 2. The method of claim 1, wherein the received data further comprises at least one of environmental conditions, and geographical data. 3. The method of claim 2, wherein calculating of the one or more v-speeds comprises continuously computing the one of more v-speeds in real-time. 4. The method of claim 2, further comprising aborting the take off if any of the received data exceeds a predetermined threshold. 5. The method of claim 2, further comprising receiving one or more estimated v-speeds from a user input device on-board the aircraft. 6. The method of claim 5, further comprising: comparing the one or more calculated v-speeds to the one or more estimated v-speeds; andgenerating an indication if a difference between the one or more calculated v-speeds and the one or more estimated v-speeds is greater than a predetermined threshold. 7. A system for controlling an aircraft during an automated take off, the system comprising: a computer processor that: receives realtime data associated with the aircraft during a take off roll, andthat calculates one or more v-speeds of the aircraft associated with the take off roll based on the realtime data; anda navigation and control system that,during the take off roll, controls the aircraft based on the one or more calculated v-speeds. 8. The system of claim 7, wherein the received data further comprises environmental conditions, and geographical data. 9. The system of claim 8, wherein the computer processor calculates the one or more v-speeds by continuously computing the one of more v-speeds in real-time. 10. The system of claim 8, wherein the navigation and control system aborts the take off if any of the received data exceeds a predetermined threshold. 11. The system of claim 8, wherein the computer processor receives one or more estimated v-speeds from a user input device on-board the aircraft. 12. The system of claim 11, wherein computer processor compares the one or more calculated v-speeds to the one or more estimated v-speeds; andgenerates an indication if a difference between the one or more calculated v-speeds and the one or more estimated v-speeds is greater than a predetermined threshold.