【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码

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⛄ 内容介绍

This project is intended to control the motion of the Unmanned Aerial Vehicle in the real world to follow a specifific trajectory smoothly and quickly. In this report, we will discuss how we design the controller and trajectory generator to reach this purpose.

In the last seven years, advances in materials, electronics, sensors and batteries have fueled a growth in the development of Micro Unmanned Aerial Vehicles (MAVs) that are between 0.1-0.5 m in length and 0.1-0.5 kg in mass [1]. A few groups have built and analyzed MAVs in the 10 cm range [2, 3]. One of the smallest is the Picoflflyer with a 60 mm propeller diameter and a mass of 3.3 g [4]. Platforms in the 50 cm range are more prevalent with several groups having built and flflown systems of this size [5–7]. In fact, there are several commercially available RC helicopters and research grade helicopters in this size range [8]. A review of the challenges in develop autonomous micro UAVs is presented in [9]. In this project, we introduce the modeling of quad rotors used in the GRASP Multiple MAV testbed to support research on coordinated, dynamic flflight of MAVs. This document is derived from the complete reference [10] which describes the approach to modeling, control and integrating off-the-shelf quad rotors.In the last seven years, advances in materials, electronics, sensors and batteries have fueled a growth in the development of Micro Unmanned Aerial Vehicles (MAVs) that are between 0.1-0.5 m in length and 0.1-0.5 kg in mass [1]. A few groups have built and analyzed MAVs in the 10 cm range [2, 3]. One of the smallest is the Picoflflyer with a 60 mm propeller diameter and a mass of 3.3 g [4]. Platforms in the 50 cm range are more prevalent with several groups having built and flflown systems of this size [5–7]. In fact, there are several commercially available RC helicopters and research grade helicopters in this size range [8]. A review of the challenges in develop autonomous micro UAVs is presented in [9]. In this project, we introduce the modeling of quad rotors used in the GRASP Multiple MAV testbed to support research on coordinated, dynamic flflight of MAVs. This document is derived from the complete reference [10] which describes the approach to modeling, control and integrating off-the-shelf quad rotors.

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第1张图片

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第2张图片

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第3张图片

⛄ 部分代码

close all;

clear all;

clc;

addpath(genpath('./'));

%% Plan path 1

disp('Planning ...');

map = load_map('maps/map1.txt', 0.1, 2, 0.25);

start = {[0.0  -4.9 0.2]};

stop  = {[6.0  18.0-1 5.0]};

% stop  = {[6.0  18.0-6 3.0]};

nquad = length(start);

for qn = 1:nquad

    tic

    path{qn} = dijkstra(map, start{qn}, stop{qn}, true);

    toc

end

if nquad == 1

    plot_path(map, path{1});

else

    % you could modify your plot_path to handle cell input for multiple robots

end

%% Plan path 3

disp('Planning ...');

map = load_map('maps/map3.txt', 0.2, 0.5, 0.25);

start = {[0.0, 5, 5.0]};

stop  = {[20, 5, 5]};

nquad = length(start);

for qn = 1:nquad

    tic

    path{qn} = dijkstra(map, start{qn}, stop{qn}, true);

    toc

end

if nquad == 1

    plot_path(map, path{1});

else

    % you could modify your plot_path to handle cell input for multiple robots

end

%% Additional init script

init_script;

%% Run trajectory

trajectory = test_trajectory(start, stop, map, path, true); % with visualization

⛄ 运行结果

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第4张图片

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第5张图片

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第6张图片

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第7张图片

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第8张图片

【无人机】基于Matlab实现无人机轨迹规划目标跟踪附论文报告和代码_第9张图片

⛄ 参考文献

[1] D. Pines and F. Bohorquez, “Challenges facing future micro air vehicle development,” AIAA Journal of Aircraft,

vol. 43, no. 2, pp. 290–305, 2006.

[2] I. Kroo, F. Prinz, M. Shantz, P. Kunz, G. Fay, S. Cheng, T. Fabian, and C. Partridge, “The mesicopter: A

miniature rotorcraft concept, phase ii interim report,” 2000.

[3] B. Hein and I. Chopra, “Hover performance of a micro air vehicle: Rotor at low reynolds number,” Journal of

the American Helicopter Society, vol. 52, no. 3, pp. 254–262, July 2007.

[4] “Proxflflyer,” http://www.proxflflyer.com.

[5] D. Gurdan, J. Stumpf, M. Achtelik, K. Doth, G. Hirzinger, and D. Rus, “Energy-effificient autonomous four

rotor flflying robot controlled at 1 khz,” in Proc. of the IEEE Int. Conf. on Robotics and Automation, Roma, Italy,

Apr. 2007.

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