Method and device for controlling aircraft for preset aircraft type based on communication and command vehicle
A technology for aircraft and command vehicles, applied in the field of electronics, can solve problems such as low control efficiency, and achieve the effects of improving control efficiency, avoiding uncertainty, and saving computation.
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Embodiment 1
[0069] The first aspect of the present invention provides a method for controlling an aircraft based on a communication command vehicle for a preset model, please refer to figure 1 , is a flowchart of a method for controlling an aircraft based on a communication command vehicle for a preset model in an embodiment of the present invention.
[0070] It should first be explained that the method can be applied to a communication command vehicle for controlling and monitoring an aircraft, or a ground station with a computer-operated control function (the ground station is a portable box with an integrated notebook computer built-in ), or a remote control terminal (such as control room, monitoring room, etc.). In other words, the above-mentioned steps in the embodiment of the present invention include the steps to be described below, and its executive body can be a communication command vehicle, so that the control method of the aircraft can be controlled in the vehicle, or it can b...
Embodiment approach
[0091] As an optional implementation manner, converting the current state information into a second physical control quantity includes:
[0092] Analyzing the correspondence between the current state information and the first physical control quantity;
[0093] According to the corresponding relationship, the current state information is converted into the second physical control quantity.
[0094] For example, there will be a corresponding relationship between the current state information and the first physical control quantity, such as the relationship between velocity and angular acceleration, the relationship between deflection angle and angular velocity, and then the corresponding relationship is converted into an angular value by designing the controller. Acceleration value, that is, the second physical control quantity.
Embodiment 2
[0096] Based on the same inventive concept as the method of controlling the aircraft based on the communication command vehicle for the preset model in the aforementioned first aspect, Embodiment 2 of the present invention also provides a control device for the aircraft, including:
[0097] The current geographic location coordinate acquisition module is used for the communication command vehicle to obtain the current geographic location coordinates of each of the aircraft in the plurality of aircraft;
[0098] The target area selection module is used for the communication command vehicle to select the target area to be controlled according to the current geographic location coordinates of each of the aircraft;
[0099] The target aircraft selection module is used for the communication command vehicle to select the target aircraft to be controlled according to the aircraft type in the target area, and the aircraft type is one of the following: fixed-wing aircraft, multi-rotor a...
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