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Online Theses Library of MG University
Category Title / Sections Scholar Branch of Study Year
Page Fig. 3-3: comparison between ANAL3 and ANAL4 values of semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005
Page Fig. 4-1: comparison between ANAL and NUM values of semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag Lila S Nair Mathematics 2005
Page Fig. 4-2: comparison between ANAL and NUM values of eccentricity decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005
Page Fig. 4-3: comparison between ANAL3 and ANAL4 values of semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag Lila S Nair Mathematics 2005
Page Fig. 5-1: comparison between ANAL and NUM values of semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005
Page Fig. 5-2: comparison between ANAL and NUM values of eccentricity decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag Lila S Nair Mathematics 2005
Page Fig. 5-3: comparison between ANAL3 and ANAL4 values of semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005
Page Fig. 6-1: comparison between ANAL4 and NUM values in semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag Lila S Nair Mathematics 2005
Page Fig. 6-2: comparison between ANAL4 and NUM values in eccentricity decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005
Page Fig. 6-3: comparison between ANAL3 and ANAL4 values in semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag Lila S Nair Mathematics 2005
Page Fig. 7-1: comparison between NUM and ANAL values in semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005
Page Fig. 7-2: comparison between NUM and ANAL4 values in eccentritity decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag Lila S Nair Mathematics 2005
Page Fig. 7-3: comparison between ANAL3 and ANAL4 values in semi-major axis after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005
Page Fig. 8-1: comparison between NUM and ANAL4 values in semi-major axis decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag Lila S Nair Mathematics 2005
Page Fig. 8-2: comparison between NUM and ANAL4 values in eccentricity decrease after 100 revolutions. (Thesis: Analytical approach using KS elements to long-term Near-Earth orbit predictions including Earth’s oblateness and air drag ) Lila S Nair Mathematics 2005



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