An aircraft controller configured to determine a period and/or distance over which deployment of a landing gear can be initiated for landing including a determined first portion during which landing gear deployment can be safely initiated and a determined second portion, closer to aircraft landing than the first portion, during which the landing gear deployment can be safely initiated in an efficient landing mode; issue a first pilot feedback when the first portion is entered by the aircraft; issue a second pilot feedback when the second portion of the determined; and initiate landing gear deployment when the aircraft is in the determined period and/or distance in response to receiving a deployment signal from the pilot.

Methods and devices for optimizing the climb of an aircraft or drone are provided. After an optimal continuous climb strategy has been determined, a lateral path is determined, in particular in terms of speeds and turn radii, based on vertical predictions computed in the previous step. Subsequently, computation results are displayed on one or more human-machine interfaces and the climb strategy is actually flown. Embodiments describe the use of altitude and speed constraints and/or settings in respect of speed and/or thrust and/or level-flight avoidance and/or gradient-variation minimization, and iteratively fitting parameters in order to make the profile of the current path coincide with the constrained profile in real time depending on the selected flight dynamics (e.g. energy sharing, constraint on climb gradient, constraint on the vertical climb rate). System (e.g. FMS) and software aspects are described.

Methods and devices for optimizing the climb of an aircraft or drone are provided. After an optimal continuous climb strategy has been determined, a lateral path is determined, in particular in terms of speeds and turn radii, based on vertical predictions computed in the previous step. Subsequently, computation results are displayed on one or more human-machine interfaces and the climb strategy is actually flown. Embodiments describe the use of altitude and speed constraints and/or settings in respect of speed and/or thrust and/or level-flight avoidance and/or gradient-variation minimization, and iteratively fitting parameters in order to make the profile of the current path coincide with the constrained profile in real time depending on the selected flight dynamics (e.g. energy sharing, constraint on climb gradient, constraint on the vertical climb rate). System (e.g. FMS) and software aspects are described.

The present application relates to a control method of an aerial vehicle. The aerial vehicle may comprise a propulsion structure for providing flight power and a spraying apparatus for spraying a material. The control method may comprise determining current target information of the aerial vehicle during a process of the aerial vehicle performing a spraying task, wherein the current target information indicates wind field strength of a downward pressure wind field generated by the propulsion structure; determining, based on the current target information, a desired relative flight altitude of the aerial vehicle corresponding to the current target information relative to the material being sprayed below the aerial vehicle; and controlling the aerial vehicle to fly toward the desired relative flight altitude.

The present application relates to a control method of an aerial vehicle. The aerial vehicle may comprise a propulsion structure for providing flight power and a spraying apparatus for spraying a material. The control method may comprise determining current target information of the aerial vehicle during a process of the aerial vehicle performing a spraying task, wherein the current target information indicates wind field strength of a downward pressure wind field generated by the propulsion structure; determining, based on the current target information, a desired relative flight altitude of the aerial vehicle corresponding to the current target information relative to the material being sprayed below the aerial vehicle; and controlling the aerial vehicle to fly toward the desired relative flight altitude.

Methods, systems, and apparatus, including computer programs encoded on a computer storage medium, are described for performing privacy-aware surveillance with a security camera drone. The drone obtains image data using an imaging device and processes the image data to detect an object external to the drone. In response to processing the image data, the drone determines multiple viewing angles indicated in the image data with respect to the object. Based on the image data and the multiple viewing angles, a first section of the area for surveillance and a second, different section of the area to be excluded from surveillance are identified. The drone determines an adjustment to at least one of the multiple viewing angles to cause the second section to be excluded from surveillance. Based on the adjustment, the drone controls the imaging device to exclude the second section from surveillance imagery obtained by the drone.

A package delivery system includes a drone that delivers a package and a package delivery control apparatus, and further includes a communication control unit that transmits a delivery code of the package to a terminal apparatus that has placed an order for delivery of the package, an irradiation control unit causes the drone to emit light in which the delivery code is superimposed when the drone arrives at a destination, and a drone control unit that, when the delivery code that the terminal apparatus has acquired by transmission from the communication control unit and the delivery code that is acquired by receiving light emitted from the drone match with each other, approves the terminal apparatus to cause the drone to perform operation of releasing the package.

A package delivery system includes a drone that delivers a package and a package delivery control apparatus, and further includes a communication control unit that transmits a delivery code of the package to a terminal apparatus that has placed an order for delivery of the package, an irradiation control unit causes the drone to emit light in which the delivery code is superimposed when the drone arrives at a destination, and a drone control unit that, when the delivery code that the terminal apparatus has acquired by transmission from the communication control unit and the delivery code that is acquired by receiving light emitted from the drone match with each other, approves the terminal apparatus to cause the drone to perform operation of releasing the package.

A system and method for integrity monitoring generates primary control output via a primary module. The primary control output is configured to be used to control an autonomous vehicle (AV). The system and method receive situational data comprising AV data and environmental data. The system and method generate, using a monitor module configured to monitor the AV, a set of fallback actions based on at least the situational data. The system and method generate, using the monitor module, a fallback status based on at least the set of fallback actions, where the fallback status is configured to correspond to a determination of whether to override the primary control output.

A method implemented by a processor associated with a movable object includes receiving a first parameter value from a user interface communicatively coupled to the movable object; determining a horizontal acceleration based on the first parameter value, wherein the horizontal acceleration is substantially zero when the first parameter value is zero; and controlling the movable object to accelerate or decelerate in accordance with the determined horizontal acceleration.