System and method for defining boundaries of a simulation of an electric aircraft
US-2023418283-A1 · Dec 28, 2023 · US
US2017316712A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2017316712-A1 |
| Application number | US-201615375292-A |
| Country | US |
| Kind code | A1 |
| Filing date | Dec 12, 2016 |
| Priority date | Apr 27, 2016 |
| Publication date | Nov 2, 2017 |
| Grant date | — |
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A control and simulation system (CSS) has a flight system configured to selectively provide flight mode of operation of an aircraft and a simulation system configured to selectively provide a simulation mode of operating the aircraft.
Opening claim text (preview).
What is claimed is: 1 . A control and simulation system (CSS), comprising: a flight system configured to selectively provide flight mode of operation of an aircraft; and a simulation system configured to selectively provide a simulation mode of operating the aircraft. 2 . The CSS of claim 1 , wherein the aircraft must be grounded prior to entering the simulation mode. 3 . The CSS of claim 1 , wherein the CSS is configured to poll a status of a weight on wheels sensor. 4 . The CSS of claim 1 , wherein the CSS is configured to determine whether an auxiliary ground power unit is connected to the aircraft. 5 . The CSS of claim 1 , wherein the CSS requires a passcode authentication prior to entering the simulation mode. 6 . The CSS of claim 1 , wherein at least one functionality of the aircraft in the flight mode is prevented from being utilized during operation of the aircraft in the simulation mode. 7 . The CSS of claim 1 , wherein the CSS is a ground-based system. 8 . The CSS of claim 7 , wherein the aircraft is simulated. 9 . The CSS of claim 7 , wherein the aircraft is configured so as not to be able to achieve flight. 10 . An aircraft, comprising: a control and simulation system (CSS), comprising: a flight system configured to selectively provide flight mode of operation of the aircraft; and a simulation system configured to selectively provide a simulation mode of operating the aircraft. 11 . The aircraft of claim 10 , wherein the aircraft must be grounded prior to entering the simulation mode. 12 . The aircraft of claim 10 , wherein the CSS is configured to poll a status of a weight on wheels sensor. 13 . The aircraft of claim 10 , wherein the CSS is configured to determine whether an auxiliary ground power unit is connected to the aircraft. 14 . The aircraft of claim 10 , wherein the CSS requires a passcode authentication prior to entering the simulation mode. 15 . The aircraft of claim 10 , wherein at least one functionality of the aircraft in the flight mode is prevented from being utilized during operation of the aircraft in the simulation mode. 16 . The aircraft of claim 10 , wherein the aircraft comprises a helicopter. 17 . The aircraft of claim 10 , wherein the aircraft comprises a tiltrotor aircraft. 18 . The aircraft of claim 10 , wherein the aircraft comprises an airplane.
by projected image ({G09B9/307,} G09B9/36 take precedence) · CPC title
including display or recording of simulated flight path · CPC title
including aircraft sound simulation · CPC title
the aircraft being a helicopter · CPC title
Simulation of view from aircraft · CPC title
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