@techreport{oai:jaxa.repo.nii.ac.jp:00044635,
 author = {武内, 澄夫 and TAKEUCHI, Sumio},
 month = {Aug},
 note = {The effect of solar radiation pressure on the motion of an artificial satellite is investigated using Lagrange’s planetary equations. The disturbing function due to the solar radiation pressure is expanded in an infinite series in terms of osculating elliptic elements. Neglecting the coupling effects between the oblateness of the earth and the solar radiation pressure, perturbations of the first order are obtained. The shadow equation is expressed by means of the quadric equation in terms of rectangular coordinates and the limits of integration are obtained by solving the shadow equation analytically. The theory has been applied to the orbits of the geostationary satellite and the balloon-type satellite, and variations of orbital elements are calculated., 資料番号: NALTR0387000, レポート番号: NAL TR-387},
 title = {人工衛星の運動に対する太陽輻射圧の影響に関する研究},
 year = {1974}
}