Flight conflict resolution method and flight conflict resolution device
A technology of flight conflict resolution and flight conflict, which is applied in the field of flight conflict resolution methods and equipment, and can solve problems such as limiting calculation efficiency and lack of global resolution methods
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Embodiment 1
[0067] figure 1 It is a schematic flowchart of Embodiment 1 of the flight conflict resolution method of the present invention. This embodiment provides a flight conflict resolution method, which can be executed by a flight conflict resolution device, and the device can be integrated into any terminal device such as a computer, a notebook computer, or a personal digital assistant (Personal Digital Assistant, PDA for short). Such as figure 1 As shown, the embodiment of the present invention provides a method for flight conflict resolution, the method includes:
[0068] S101. Obtain a flight conflict situation estimation model according to the four-dimensional trajectory of the aircraft to be optimized. The flight conflict situation estimation model includes a plurality of individuals, and each of the plurality of individuals includes the take-off delay time of all aircraft to be optimized. different.
[0069] Due to the realization of track information sharing under the four-...
Embodiment 2
[0083] Figure 4 It is a schematic flowchart of Embodiment 2 of the flight conflict resolution method of the present invention. Such as Figure 4 As shown, the method includes:
[0084] S401. Establish a flight conflict situation estimation model.
[0085] In this embodiment, first set the take-off delay time of all aircraft to be optimized as a set Among them, δ i Indicates the take-off delay time of the i-th aircraft to be optimized, and n indicates the total number of all aircraft to be optimized. For each variable δ i , must satisfy the constraint of value range: δ i ∈[0,δ max ],δ max is the objectively allowed maximum takeoff delay time. The invention takes the take-off delay time of the aircraft to be optimized as an adjustment parameter, and optimizes the flight conflict situation estimation model in combination with the take-off delay time of all the aircraft to be optimized, which is a flight conflict resolution solution. Here, the coding of the aircraft ...
Embodiment 3
[0141] Figure 7 It is a schematic structural diagram of Embodiment 3 of the flight conflict resolution device of the present invention. The present invention provides a flight conflict resolution device, which can be integrated into any terminal device such as a computer, a notebook computer or a PDA. Such as Figure 7 As shown, the flight conflict resolution device 70 includes: an acquisition module 71 , a calculation module 72 , a variation module 73 and an update module 74 .
[0142] Wherein, the obtaining module 71 is used to obtain the flight conflict situation estimation model according to the four-dimensional trajectory of the aircraft to be optimized, the flight conflict situation estimation model includes a plurality of individuals, and each individual in the plurality of individuals includes the take-off delay time of all aircraft to be optimized, And different individuals are different; the calculation module 72 is used to obtain the corresponding objective funct...
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