Abstract: A method S100 can include: determining a set of inputs Silo; determining a vehicle state estimate S120; determining a vehicle command based on the vehicle state estimate S130; and optionally controlling the vehicle based on the vehicle command S140. However, the method S100 can additionally or alternatively include any other suitable elements. The method S100 functions to facilitate vehicle reversal and/or tractable vehicle control (e.g., during reversal). Additionally or alternatively, the method can function to reduce and/or eliminate unrecoverable vehicle state incidence during vehicle reversal (a.k.a., vehicle backing). Additionally or alternatively, the method can function to autonomously augment and/or assist vehicle control (e.g., during vehicle reversal).

Abstract: A method S100 can include: determining a set of inputs S110; determining a vehicle state estimate S120; determining a vehicle command based on the vehicle state estimate S130; and optionally controlling the vehicle based on the vehicle command S140. However, the method S100 can additionally or alternatively include any other suitable elements. The method S100 functions to facilitate vehicle reversal and/or tractable vehicle control (e.g., during reversal). Additionally or alternatively, the method can function to reduce and/or eliminate unrecoverable vehicle state incidence during vehicle reversal (a.k.a., vehicle backing). Additionally or alternatively, the method can function to autonomously augment and/or assist vehicle control (e.g., during vehicle reversal).

Abstract: A method S100 can include: determining a set of inputs Silo; determining a vehicle state estimate S120; determining a vehicle command based on the vehicle state estimate S130; and optionally controlling the vehicle based on the vehicle command S140. However, the method S100 can additionally or alternatively include any other suitable elements. The method S100 functions to facilitate vehicle reversal and/or tractable vehicle control (e.g., during reversal). Additionally or alternatively, the method can function to reduce and/or eliminate unrecoverable vehicle state incidence during vehicle reversal (a.k.a., vehicle backing). Additionally or alternatively, the method can function to autonomously augment and/or assist vehicle control (e.g., during vehicle reversal).

Abstract: An infrared sensing gesture recognition method, characterized in that the recognition method adopts multiple infrared light emitting units, and each infrared light emitting unit is loaded with pulse signals on different frequencies, then, one or more infrared receiving units for receiving signals are used to receive infrared reflected signals loaded with corresponding frequencies emitted from different infrared light emitting units, and the infrared reflected signal corresponds to the infrared light emitting unit with the corresponding frequency by identifying the frequency of pulse signal loaded in the infrared reflected signal, so as to determine the physical location of infrared light emitting unit, and to judge the movement trajectory of gesture.

Abstract: An aircraft cockpit view enhancement system and method. The aircraft cockpit view enhancement system has: front-position, left-position and right-position camera devices. The front-position camera device is arranged between a driver's eye position point and an aircraft windshield pillar, with a photographing angle directly facing the aircraft windshield pillar, and the left-position and right-position camera devices are respectively arranged at a left side and a right side of the aircraft windshield pillar, with photographing angles respectively pointing to the right side and the left side deviated from the aircraft windshield pillar. An image processing device for performing image synthesis and image registration on a front-position image, a left-position image and a right-position image photographed by the front-position camera device, the left-position camera device and the right-position camera device, to obtain an image of a region shielded by the aircraft windshield pillar.

Abstract: An aircraft cockpit view enhancement system and method. The aircraft cockpit view enhancement system has: front-position, left-position and right-position camera devices. The front-position camera device is arranged between a driver's eye position point and an aircraft windshield pillar, with a photographing angle directly facing the aircraft windshield pillar, and the left-position and right-position camera devices are respectively arranged at a left side and a right side of the aircraft windshield pillar, with photographing angles respectively pointing to the right side and the left side deviated from the aircraft windshield pillar. An image processing device for performing image synthesis and image registration on a front-position image, a left-position image and a right-position image photographed by the front-position camera device, the left-position camera device and the right-position camera device, to obtain an image of a region shielded by the aircraft windshield pillar.

Abstract: Systems (100) and methods (1700) for providing a marker (102). The methods comprise forming a magnetic core (200) having a bone shape defined by two end portions (208, 212) and a center potion (210) disposed between the two end portions. The end portions each have a cross-sectional area larger than a cross-sectional area of the center portion. A coil (224) is disposed around the center portion. The coil is coupled to a passive electronic component (206) so as to form a resonator. The resonator is disposed in a housing (126) of the marker. The resonator resonates when an interrogation signal is produced by a transmitter circuit (112) located remote from and in proximity to the marker, whereby a variation in a magnetic field occurs.

Abstract: Systems (100) and methods (1700) for providing a marker (102). The methods comprise forming a magnetic core (200) having a bone shape defined by two end portions (208, 212) and a center potion (210) disposed between the two end portions. The end portions each have a cross-sectional area larger than a cross-sectional area of the center portion. A coil (224) is disposed around the center portion. The coil is coupled to a passive electronic component (206) so as to form a resonator. The resonator is disposed in a housing (126) of the marker. The resonator resonates when an interrogation signal is produced by a transmitter circuit (112) located remote from and in proximity to the marker, whereby a variation in a magnetic field occurs.