Genetic Algorithm and Greedy Strategy-Based Multi-Mission-Point Route Planning for Heavy-Duty Semi-Rigid Airship

被引:7
作者
Hu, Shaoxing [1 ]
Wang, Bingke [1 ]
Zhang, Aiwu [2 ,3 ]
Deng, Yiming [4 ]
机构
[1] Beihang Univ, Sch Mech Engn & Automat, Beijing 100191, Peoples R China
[2] Capital Normal Univ, Key Lab 3D Informat Acquisit & Applicat, Minist Educ, Beijing 100048, Peoples R China
[3] Capital Normal Univ, Ctr Geog Environm Res & Educ, Beijing 100048, Peoples R China
[4] Michigan State Univ, Nondestruct Evaluat Lab, Dept Elect & Comp Engn, Coll Engn, E Lansing, MI 48824 USA
关键词
multi-mission-point; route planning; minimum turning radius; optimal flight sequence; shortest route; OPTIMIZATION;
D O I
10.3390/s22134954
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
The large volume and windward area of the heavy-duty semi-rigid airship (HSA) result in a large turning radius when the HSA passes through every mission point. In this study, a multi-mission-point route planning method for HSA based on the genetic algorithm and greedy strategy is proposed to direct the HSA maneuver through every mission point along the optimal route. Firstly, according to the minimum flight speed and the maximum turning slope angle of the HSA during turning, the minimum turning radius of the HSA near each mission point is determined. Secondly, the genetic algorithm is used to determine the optimal flight sequence of the HSA from the take-off point through all the mission points to the landing point. Thirdly, based on the optimal flight sequence, the shortest route between every two adjacent mission points is obtained by using the route planning method based on the greedy strategy. By determining the optimal flight sequence and the shortest route, the optimal route for the HSA to pass through all mission points can be obtained. The experimental results show that the method proposed in this study can generate the optimal route with various conditions of the mission points using simulation studies. This method reduces the total voyage distance of the optimal route by 18.60% on average and improves the flight efficiency of the HSA.
引用
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页数:20
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