Flight control and energy guidance system (FCS&EGS) status monitoring graphical user interface for electronic devices

Abstract

1. The name of the design product: electronic device flight control and energy system (FCS & EGS) state monitoring graphical user interface. 2. The use of the design product: for an electronic device. 3. The design points of the design product: in the graphical user interface. 4. The picture or photo that best indicates the design points: front view. 5. The electronic device is of conventional design, and other views are omitted. 6. The use of the graphical user interface: for real-time display of flight control state, energy parameters, and support for flight control channel, flight control mode switching, and other interactive operations. Wherein, FCS represents the flight control system; EGS represents the energy system; Min Temp represents the minimum temperature; SOC represents the remaining power; SOP represents the power state; RT represents the running time; PSP on the fuselage represents the power supply point; "% / V / ℃" on the fuselage module respectively represents the voltage ratio / voltage value / temperature of the energy module; the cross mark (C / R) represents the state indication of "C channel" and "R channel"; SSU represents the signal processing unit; UP / DN represents the position / threshold parameter related to flight control; L / R represents the left / right position / parameter of the flight control subsystem; FCC represents the flight control computer, "1 / 2 / 3" corresponds to different control channels of the flight control system, and "B" is the backup channel; Control Mode represents the flight control mode for switching control logic; INFO represents the system detail information display.

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