[{"title":"( 9 个子文件 12.18MB ) 卫星轨道绝对动力学(龙格库塔积分方法)","children":[{"title":"卫星轨道绝对动力学(龙格库塔积分方法)","children":[{"title":"离心率为0","children":[{"title":"STK_real.mat <span style='color:#111;'> 3.64MB </span>","children":null,"spread":false},{"title":"输入初始位置速度.csv <span style='color:#111;'> 5.43MB </span>","children":null,"spread":false},{"title":"orbitdynamic_main.m <span style='color:#111;'> 1.53KB </span>","children":null,"spread":false},{"title":"orbitdynamics_runge_kutta.m <span style='color:#111;'> 1.49KB </span>","children":null,"spread":false}],"spread":true},{"title":"离心率为0.6","children":[{"title":"satelliteposition.mat <span style='color:#111;'> 3.35MB </span>","children":null,"spread":false},{"title":"捕获.PNG <span style='color:#111;'> 8.15KB </span>","children":null,"spread":false},{"title":"orbitdynamic_main.m <span style='color:#111;'> 1.79KB </span>","children":null,"spread":false},{"title":"Satellite1 J2000 Position Velocity.csv <span style='color:#111;'> 7.65MB </span>","children":null,"spread":false},{"title":"orbitdynamics_runge_kutta.m <span style='color:#111;'> 1.49KB </span>","children":null,"spread":false}],"spread":true}],"spread":true}],"spread":true}]