A resource allocation and flight route optimization method for unmanned aerial vehicle relay system
A relay system and flight route technology, applied in the field of communication, can solve problems such as the inability to adjust user weights and the inability to maximize the weighted sum of user rates, and achieve a wide range of applications
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Embodiment 1
[0106] Such as figure 1 As shown, a method for resource allocation and flight route optimization of an unmanned aerial vehicle relay system includes the following steps:
[0107] Step S1: Set the initial UAV flight trajectory Q l , let the initial objective function value Cycle times l=0, error threshold ε=10 -3 , the bandwidth is A, the transmit power is P, and the given bandwidth and transmit power are allocated as {A,P};
[0108] Step S2: Establish a model of the UAV relay system, use the given bandwidth and transmit power to allocate {A,P} and the initial UAV flight trajectory Q l Solve to get the optimal solution of UAV flight trajectory bandwidth and transmission power distribution {A l+1 ,P l +1};
[0109] Step S3: Use the given bandwidth and transmit power to allocate {A, P} to the UAV flight trajectory Q l Optimize and solve to get the optimal solution Q of UAV flight trajectory l+1 and get the objective function value
[0110] Step S4: make l=l+1; and ju...
Embodiment 2
[0198] Such as figure 2 As shown, in this embodiment, by jointly optimizing the power, bandwidth and trajectory respectively; given the flight trajectory of the UAV, optimize the power and bandwidth; In the three cases, the trend graph of the information throughput changing with the flight time in the three cases is obtained, and the average average transmit power p=10dBm.
[0199] Depend on figure 2 It can be seen that the optimization strategy of jointly optimizing power, bandwidth and trajectory proposed in this paper has obvious performance gain.
[0200] The same or similar reference numerals correspond to the same or similar components;
[0201] The terms describing the positional relationship in the drawings are only for illustrative purposes and cannot be interpreted as limitations on this patent;
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