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Question
I am using Aerospace toolbox function lambertMR but I'm unable to run this code.
% Define given parameters R1 = 6378.137 + 300; % Radius of OTV circular orbit (km) i1 = deg2rad(30); % Inclination ...
3 years ago | 1 answer | 0
1
answerQuestion
unable to run the program becuase of matrix multiplication error, also need to add a 3d earth around which the plot of orbit displayed.
clc close all clear all % Constants mu = 398600.4418; % km^3/s^2 RE = 6378.137; % km wE = 7.2921158553e-5; % rad/s % Orb...
3 years ago | 1 answer | 0
