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PengLu / 使用kinodynamic RRTStar算法规划轨迹

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function dmdt = dmdt(~,m)
%DMDT
% DMDT = DMDT(M1,M2,M3,M4,M5,M6,M7,M8,M9,M10,M11,M12)
% This function was generated by the Symbolic Math Toolbox version 8.0.
% 12-Jul-2018 11:32:56
%
% 以下被注释for循环程序可以打印出:
% m1 = m(1);
% .
% .
% .
% m12 = m(12);
% for i = 1:12
% fprintf('m%d = m(%d);',i,i)
% fprintf('\n')
% end
m1 = m(1);
m2 = m(2);
% m3 = m(3);
m4 = m(4);
m5 = m(5);
m6 = m(6);
m7 = m(7);
m8 = m(8);
m9 = m(9);
m10 = m(10);
m11 = m(11);
m12 = m(12);
dmdt = [m4;m5;m6;m1.*1.098649095807376e-7+m5.*6.6291752e-4+m10.*2.0+1.0./5.0e2;m2.*1.098649095807376e-7-m4.*6.6291752e-4+m11.*2.0+1.0./5.0e2;m12.*2.0+1.0./5.0e2;m10.*(-1.098649095807376e-7);m11.*(-1.098649095807376e-7);0.0;-m7+m11.*6.6291752e-4;-m8-m10.*6.6291752e-4;-m9];

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https://gitee.com/olupengo/kinodynamic-RRTStar-for-landing-on-small-body.git
git@gitee.com:olupengo/kinodynamic-RRTStar-for-landing-on-small-body.git
olupengo
kinodynamic-RRTStar-for-landing-on-small-body
使用kinodynamic RRTStar算法规划轨迹
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