源码文件
==== Aerodynamic Analysis Output File ==== Surface Area of the Fuselage = 139.18 ft^2 Wetted Area of the Aircraft …
aircraft 源代码
探索AIRcraft技术，掌握未来航空电子系统的核心。本页面汇集了16个精选资源，涵盖从基础理论到高级应用的全方位知识。无论是无人机控制、飞行器导航还是空中交通管理，这里都有你所需的专业资料。深入学习AIRcraft相关技术，不仅能够提升个人技能，还能为您的项目带来创新解决方案。…
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源码文件
function blkStruct = slblocks blkStruct.Name = ['Aircraft Library']; blkStruct.OpenFcn = 'airlib'; %blkStruct.MaskDisplay = '';
源码文件
%Initial values of the constants are given g = 32.2; % Acceleration due to gravity (ft/sec^2) tauc = 5; % Correlation time…
源码文件
% SIXDOFVM Calculate aircraft variable-mass rigid-body six-degrees-of-freedom % equations of motion using MATLAB ODE45 solver. …
源码文件
% SIXDOF Calculate aircraft fixed-mass rigid-body six-degrees-of-freedom % equations of motion using MATLAB ODE45 solver. % % …
源码文件
clear all close all thetaA= 1.33; % antenna azimuth beamwidth in degrees thetaE = 11; % antenna elevation beamwidth in degrees …
源码文件
clear all close all thetaA= 1.33; % antenna azimuth beamwidth in degrees thetaE = 11; % antenna elevation beamwidth in degrees …
源码文件
clear all close all thetaA= 1.33; % antenna azimuth beamwidth in degrees thetaE = 11; % antenna elevation beamwidth in degrees …
源码文件
/* * @(#)VectorEditor.java 1.1 00/02/10 * * Copyright (c) 1999 Sun Microsystems, Inc. All Rights Reserved. * * Sun grants you…
源码文件
clear all close all thetaA= 1.33; % antenna azimuth beamwidth in degrees thetaE = 11; % antenna elevation beamwidth in degrees …