THE 2-BODY PROBLEM WITH DRAG AND RADIATION PRESSURE

被引:22
作者
MAVRAGANIS, AG
MICHALAKIS, DG
机构
[1] Dept. of Engineering Science, Section of Mechanics, National Technical University of Athens
关键词
RADIATION PRESSURE; ATMOSPHERIC DRAG;
D O I
10.1007/BF00692013
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The Kepler problem including radiation pressure and drag is treated. The equation of the orbit is derived and the scalar and vector integrals of motion are obtained by direct operation on the vector form of the equation of motion.
引用
收藏
页码:393 / 403
页数:11
相关论文
共 6 条
[1]  
Brouwer D., Hori G., Theoretical evaluation of atmospheric drag effects in the motion of an artificial satellite, The Astronomical Journal, 66, (1961)
[2]  
Danby J.M.A., Fundamentals of Celestical Mechanics, (1962)
[3]  
Leach P.G.L., J. Phys. A: Math. Gen., 20, pp. 1997-2002, (1987)
[4]  
Jezewski D., Mittleman D., Int. J. Non-Linear Mech., 18, 2, pp. 119-124, (1983)
[5]  
Mittleman D., Jezewski D., Celest. Mech., 28, pp. 401-413, (1982)
[6]  
Mavraganis A.G., Celest. Mech., 51, pp. 395-405, (1991)