Assisted flight computer program and method

1. An avionics system for an aircraft, the avionics system comprising:

an input for receiving an initiation signal from a dedicated emergency input device;

an autopilot for automatically controlling certain aspects of the aircraft;

a transmitter for sending transmissions from the aircraft;

an assisted flight program, responsive to the initiation signal from the dedicated emergency input device, and configured to—

engage the autopilot to stabilize flight of the aircraft,

alert a ground controller, through the transmitter, that the aircraft is in an emergency situation, and

assist a passenger of the aircraft in controlling the aircraft, and

a display configured to present conventional flight information and replace the conventional flight information with simplified flight information upon reception of the initiation signal.

2. The avionics system of claim 1 , wherein the assisted flight program is further operable to automatically control a function of the aircraft to prepare the aircraft for landing.

3. The avionics system of claim 2 , wherein the automatically controlling a function step is selected from the group consisting of: changing a frequency of a radio on the aircraft; setting a heading of the aircraft; setting an altitude of the aircraft; setting a holding pattern of the aircraft; configuring an auto pilot of the aircraft; performing a pre-landing checklist; setting an approach of the aircraft; setting an air speed of the aircraft; setting or changing a flight plan for the aircraft; drawing a visual flight rules (VFR) approach of the aircraft; setting a barometric pressure correction setting of the aircraft; changing a navigation setting of the aircraft; setting a transponder code; and setting a descent or climb rate.

4. The avionics system as set forth in claim 1 , wherein the avionics system alerts the ground controller by changing a transponder setting of the aircraft to an emergency code.

5. The avionics system as set forth in claim 1 , wherein the avionics system alerts the ground controller by changing a radio on the aircraft to an emergency frequency and then prompting the passenger to transmit an emergency message to the ground controller.

6. The avionics system as set forth in claim 5 , wherein the prompting step includes the step of displaying the emergency message on the display in the aircraft and prompting the passenger to read the emergency message over the radio.

7. The avionics system as set forth in claim 5 , further including a speaker operable to generate sound, wherein the assisted flight program is further operable to execute a text-to-speech (TTS) program to audibly present the prompts to the passenger using the speaker.

8. The avionics system as set forth in claim 1 , wherein the assisted flight program is further operable to determine a suitable airport at which to land the aircraft and then prompt the passenger to direct the aircraft to the airport.

9. The avionics system as set forth in claim 8 , wherein the assisted flight program takes into account a factor selected from the group consisting of a distance between the aircraft and the airport; approaches available at the airport; fuel remaining in the aircraft; altitude of the aircraft; weather; terrain near the aircraft; terrain near the airport; and performance characteristics of the aircraft when determining the suitable airport.

10. The avionics system as set forth in claim 1 , wherein the display is operable to present a visual representation of a device to be controlled by the passenger along with control instructions to assist the passenger in controlling the aircraft.

11. The avionics system as set forth in claim 1 , further including a microphone operable to receive an audible command from the passenger, wherein the assisted flight program is further operable to execute an automatic speech recognition (ASR) program to recognize the audible command from the passenger and automatically perform an associated task.