Methods and apparatus for reducing anxiety during travel
First Claim
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1. A system comprising:
- a portable electronic device;
one or more accelerometers, the one or more accelerometers configured to generate acceleration data based on a flight of an airplane, the acceleration data being indicative of acceleration along a first axis, a second axis, and a third axis; and
computer program code stored in the portable electronic device that, when executed by the portable electronic device, causes the portable electronic device to;
monitor the acceleration data generated by the one or more accelerometers during the flight of the airplane; and
display a representation of the acceleration data generated by the one or more accelerometers in relation to a maximum safe acceleration of the airplane;
wherein the first axis, the second axis, and the third axis are each orthogonal to the other two axes, and the maximum safe acceleration is an acceleration beyond which damage to the airplane in flight is expected, andwherein the one or more accelerometers are disposed within the portable electronic device, and the computer program code stored in the portable electronic device, when executed by the portable electronic device, further causes the portable electronic device to monitor acceleration of the airplane responsive to the acceleration data generated by the one or more accelerometers during the flight of the airplane.
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Abstract
In some embodiments, a system is provided that includes a portable electronic device; and an application executable on the portable electronic device, the application including computer program code that (a) monitors acceleration data during a flight of an airplane; and (b) displays a representation of the acceleration data in relation to a threshold acceleration of the airplane. Numerous other aspects are provided.
24 Citations
18 Claims
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1. A system comprising:
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a portable electronic device; one or more accelerometers, the one or more accelerometers configured to generate acceleration data based on a flight of an airplane, the acceleration data being indicative of acceleration along a first axis, a second axis, and a third axis; and computer program code stored in the portable electronic device that, when executed by the portable electronic device, causes the portable electronic device to; monitor the acceleration data generated by the one or more accelerometers during the flight of the airplane; and display a representation of the acceleration data generated by the one or more accelerometers in relation to a maximum safe acceleration of the airplane; wherein the first axis, the second axis, and the third axis are each orthogonal to the other two axes, and the maximum safe acceleration is an acceleration beyond which damage to the airplane in flight is expected, and wherein the one or more accelerometers are disposed within the portable electronic device, and the computer program code stored in the portable electronic device, when executed by the portable electronic device, further causes the portable electronic device to monitor acceleration of the airplane responsive to the acceleration data generated by the one or more accelerometers during the flight of the airplane. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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8. An apparatus, comprising:
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a portable electronic device; one or more accelerometers disposed in the portable electronic device, the one or more accelerometers configured to generate acceleration data based on a flight of an aircraft, the acceleration data representative of a magnitude of instantaneous acceleration; and a display screen coupled to the portable electronic device, wherein the portable electronic device is configured to correlate instantaneous magnitudes of acceleration experienced over time by the aircraft carrying the portable electronic device based on the acceleration data generated by the one or more accelerometers during the flight of the aircraft, wherein the portable electronic device is further configured to display, on the display screen, a representation of the instantaneous magnitudes of acceleration over time in relation to a threshold acceleration tolerance level of the aircraft; wherein an acceleration of the aircraft greater than the threshold acceleration tolerance level of the aircraft can damage the aircraft in flight; and wherein the portable electronic device is configured to monitor acceleration of the aircraft responsive to the acceleration data generated by the one or more accelerometers during the flight of the aircraft. - View Dependent Claims (9, 10, 11)
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12. A method of reducing anxiety during a flight, comprising:
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providing a portable electronic device having computer program code stored therein that, when executed by the portable electronic device, causes the portable electronic device to; monitor acceleration data during the flight of an airplane; and display a representation of the acceleration data in relation to a threshold acceleration tolerance level of the airplane; operating one or more accelerometers during the flight of the airplane, such that the one or more accelerometers generate the acceleration data; monitoring, by the portable electronic device, the acceleration data during the flight of the airplane; and displaying, by the portable electronic device, the representation of the acceleration data in relation to the threshold acceleration tolerance level of the airplane, wherein an acceleration of the airplane greater than the threshold acceleration tolerance level of the airplane can damage the airplane in flight, and wherein the one or more accelerometers are disposed within the portable electronic device, and the computer program code stored in the portable electronic device, when executed by the portable electronic device, further causes the portable electronic device to monitor acceleration of the airplane responsive to the acceleration data generated by the one or more accelerometers during the flight of the airplane. - View Dependent Claims (13, 14, 15, 16, 17, 18)
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Specification