Method and device for controlling aircraft in target area based on ground station
A target area and ground station technology, applied in attitude control, non-electric variable control, control/adjustment system, etc., can solve the problem of low control efficiency, achieve the effect of improving control efficiency, avoiding uncertainty, and saving calculation amount
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Embodiment 1
[0072] The first aspect of the present invention provides a method for controlling an aircraft in a target area based on a ground station, please refer to figure 1 , is a flowchart of a method for controlling an aircraft in a target area based on a ground station in an embodiment of the present invention.
[0073] 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 be equipped with a computer The gr...
Embodiment approach
[0095] As an optional implementation manner, converting the current state information into a second physical control quantity includes:
[0096]Analyzing the correspondence between the current state information and the first physical control quantity;
[0097] According to the corresponding relationship, the current state information is converted into the second physical control quantity.
[0098] 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
[0100] Based on the same inventive concept as the method for controlling an aircraft based on a ground station in a target area in the aforementioned first aspect, Embodiment 2 of the present invention also provides a control device for an aircraft, including:
[0101] The basic geographic location coordinate acquisition module is used for the ground station to obtain the basic geographic location coordinates of markers in the basic area;
[0102] The target area forming module is used for the ground station to form a circular target area with the coordinates of the basic geographic location as the coordinate origin and the distance H as the target radius;
[0103] The current geographic location coordinate acquisition module is used for the ground station to obtain the current geographic location coordinates of each of the aircraft in the target area;
[0104] The target aircraft selection module is used for the ground station to select the target aircraft to be controlled ac...
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