Abstract: The present disclosure provides a viewing angle switching structure, a display device and a viewing angle switching method. The viewing angle switching structure includes a plurality of viewing angle switching units corresponding to pixels on a display panel. Each viewing angle switching unit includes: an accommodation cavity; a first solution layer and a second solution layer in the accommodation cavity, a liquid interface being formed between the first and the second solution layers; and an electric field driving unit configured to generate a driving electric field to be applied to the accommodation cavity. The first solution layer has a refractive index different from the second solution layer. The first solution layer includes a transparent conductive solution and the second solution layer includes a transparent non-conductive solution. A shape of the liquid interface between the first and the second solution layers is changeable under the effect of the driving electric field.

Abstract: A surface texture identification display device and a surface texture identification method are provided. The surface texture identification method has a first surface for being contacted with a textured surface. The surface texture identification display device includes: an opaque backplane; a plurality of electroluminescent pixel units, located between the opaque backplane and the first surface and arranged in a plurality of rows extending in a first direction and a plurality of columns extending in a second direction; an image sensor located on a side of the opaque backplane away from the first surface; and a plurality of imaging pinholes, passing through the opaque backplane and configured to image the textured surface onto the image sensor. In a plan view of the surface texture identification display device, the plurality of pixel units and the plurality of imaging pinholes are located within an effective display region.

Abstract: The present disclosure provides a display panel, a method for driving the same and a display device. A pixel circuit of the display panel includes a storage capacitor, a driving transistor, an initialization module configured to apply an initial voltage to a first end of the storage capacitor via a current-level gate scanning line within an initialization time period, a compensation module, a data writing module, a resetting module configured to enable the current-level gate scanning line to be electrically connected to a second end of the storage capacitor within a light-emitting time period, and a light-emitting control module. The driving transistor is in an on state within the light-emitting time period, so as to drive a light-emitting element to emit light.

Abstract: A loss-of-control prevention and recovery automatic control system of an aircraft is provided having a plurality of flight control mode, including a nominal flight control mode, a loss-of-control prevention control mode, a loss-of-control arrest control mode, and a nominal flight restoration control mode, as well as a supervisory control system capable of monitoring the flight states and flight events of the aircraft and determining which flight control mode to activate.

Abstract: There are provided a shift register, a gate driving circuit and a relevant display device, comprising a first node controlling module (1), a second node controlling module (2), a third node controlling module (3), a first outputting module (4) and a second outputting module (5). The first node controlling module (1) adjust a potential of a first node (A), the second node controlling module (2) adjust a potential of a second node (B), the third node controlling module (3) adjust a potential of a third node (C), the first outputting module (4) adjust a potential of a driving signal output terminal (Output), and the second outputting module (5) adjusts the potential of the driving signal output terminal (Output).

Abstract: The present disclosure provides a display panel, a method for driving the same and a display device. A pixel circuit of the display panel includes a storage capacitor, a driving transistor, an initialization module configured to apply an initial voltage to a first end of the storage capacitor via a current-level gate scanning line within an initialization time period, a compensation module, a data writing module, a resetting module configured to enable the current-level gate scanning line to be electrically connected to a second end of the storage capacitor within a light-emitting time period, and a light-emitting control module. The driving transistor is in an on state within the light-emitting time period, so as to drive a light-emitting element to emit light.

Abstract: There are provided a shift register, a gate driving circuit and a relevant display device, comprising a first node controlling module (1), a second node controlling module (2), a third node controlling module (3), a first outputting module (4) and a second outputting module (5). The first node controlling module (1) adjust a potential of a first node (A), the second node controlling module (2) adjust a potential of a second node (B), the third node controlling module (3) adjust a potential of a third node (C), the first outputting module (4) adjust a potential of a driving signal output terminal (Output), and the second outputting module (5) adjusts the potential of the driving signal output terminal (Output).

Abstract: A multi-modal vehicle (“MMV”) 20a-20d. The MMV 20a-20d includes a fuselage 22 and a chassis 26 supporting at least three wheels 44 having deployed and stowed states. Extending away from the fuselage 22 is a canard wing system 28 and a main wing system 30. The main wing system 30 includes an inboard portion 134 and an outboard portion 132. The inboard portion 134 is pivotally connected to the fuselage 22; the outboard portion 132 is pivotally connected to the inboard portion 134. The MMV 20a-20d further includes a vertical thrust system 32 comprising a pair of ducted fans 100 that are incorporated into the fuselage 22, and a dual-use thrust system 34 that is configured to transition between a first position for supplying vertical thrust and a second position for supplying a horizontal thrust. A controller 42 is configured to control the MMV operations, reconfigurations, or transitions.

Abstract: A multi-modal vehicle (“MMV”) 20a-20d. The MMV 20a-20d includes a fuselage 22 and a chassis 26 supporting at least three wheels 44 having deployed and stowed states. Extending away from the fuselage 22 is a canard wing system 28 and a main wing system 30. The main wing system 30 includes an inboard portion 134 and an outboard portion 132. The inboard portion 134 is pivotally connected to the fuselage 22; the outboard portion 132 is pivotally connected to the inboard portion 134. The MMV 20a-20d further includes a vertical thrust system 32 comprising a pair of ducted fans 100 that are incorporated into the fuselage 22, and a dual-use thrust system 34 that is configured to transition between a first position for supplying vertical thrust and a second position for supplying a horizontal thrust. A controller 42 is configured to control the MMV operations, reconfigurations, or transitions.

Abstract: A motorized drive system and method for articulating an articulated joint having a motor and an elastic cable. The elastic cable is operatively connected to both the motor and the articulated joint such that the motor articulates the joint via the elastic cable. In addition, the elastic cable is adapted to be sufficiently elastic such that the motorized drive system is configured to use one motor for each degree of freedom through which the articulated joint moves.

Abstract: A motorized drive system and method for articulating an articulated joint having a motor and an elastic cable. The elastic cable is operatively connected to both the motor and the articulated joint such that the motor articulates the joint via the elastic cable. In addition, the elastic cable is adapted to be sufficiently elastic such that the motorized drive system is configured to use one motor for each degree of freedom through which the articulated joint moves.

Abstract: A six degree-of-freedom trajectory linearization controller (TLC) architecture (30) for a fixed-wing aircraft (46) is set forth. The TLC architecture (30) calculates nominal force and moment commands by dynamic inversion of the nonlinear equations of motion. A linear time-varying (LTV) tracking error regulator provides exponential stability of the tracking error dynamics and robustness to model uncertainty and error. The basic control loop includes a closed-loop, LTV stabilizing controller (12), a pseudo-inverse plant model (14), and a nonlinear plant model(16). Four of the basic control loops (34, 36, 40, 42) are nested to form the TLC architecture (30).

Abstract: A multi-modal vehicle (“MMV”) 20a-20d. The MMV 20a-20d includes a fuselage 22 and a chassis 26 supporting at least three wheels 44 having deployed and stowed states. Extending away from the fuselage 22 is a canard wing system 28 and a main wing system 30. The main wing system 30 includes an inboard portion 134 and an outboard portion 132. The inboard portion 134 is pivotally connected to the fuselage 22; the outboard portion 132 is pivotally connected to the inboard portion 134. The MMV 20a-20d further includes a vertical thrust system 32 comprising a pair of ducted fans 100 that are incorporated into the fuselage 22, and a dual-use thrust system 34 that is configured to transition between a first position for supplying vertical thrust and a second position for supplying a horizontal thrust. A controller 42 is configured to control the MMV operations, reconfigurations, or transitions.

Abstract: A six degree-of-freedom trajectory linearization controller (TLC) architecture (30) for a fixed-wing aircraft (46) is set forth. The TLC architecture (30) calculates nominal force and moment commands by dynamic inversion of the nonlinear equations of motion. A linear time-varying (LTV) tracking error regulator provides exponential stability of the tracking error dynamics and robustness to model uncertainty and error. The basic control loop includes a closed-loop, LTV stabilizing controller (12), a pseudo-inverse plant model (14), and a nonlinear plant model(16). Four of the basic control loops (34, 36, 40, 42) are nested to form the TLC architecture (30).