基于SGP4的卫星轨道计算程序

[{"title":"（ 13 个子文件 4.89MB ） 基于SGP4的卫星轨道计算程序","children":[{"title":"SGP4","children":[{"title":"actan.m <span style='color:#111;'> 293B </span>","children":null,"spread":false},{"title":"An Improved Analytical Drag Theory for the Artificial Satellite Problem.pdf <span style='color:#111;'> 567.16KB </span>","children":null,"spread":false},{"title":"modulus.m <span style='color:#111;'> 369B </span>","children":null,"spread":false},{"title":"Convert_Sat_State.m <span style='color:#111;'> 402B </span>","children":null,"spread":false},{"title":"test_sgp4.m <span style='color:#111;'> 3.24KB </span>","children":null,"spread":false},{"title":"tle.txt <span style='color:#111;'> 138B </span>","children":null,"spread":false},{"title":"sgp4.m <span style='color:#111;'> 6.80KB </span>","children":null,"spread":false},{"title":"Solution of the Problem of Artificial Satellite Theory without Drag.pdf <span style='color:#111;'> 1.01MB </span>","children":null,"spread":false},{"title":"spacetrk.pdf <span style='color:#111;'> 473.57KB </span>","children":null,"spread":false},{"title":"On the Representation of Air Density in Satellite Deceleration Equations by Power Functions with Integral Exponents.pdf <span style='color:#111;'> 1.47MB </span>","children":null,"spread":false},{"title":"General Perturbations Theories Derived from the 1965 Lane Drag Theory.pdf <span style='color:#111;'> 1.65MB </span>","children":null,"spread":false},{"title":"fmod2p.m <span style='color:#111;'> 260B </span>","children":null,"spread":false}],"spread":false},{"title":"license.txt <span style='color:#111;'> 1.28KB </span>","children":null,"spread":false}],"spread":true}]