| Category |
Title / Sections |
Scholar |
Branch of Study |
Year |
| Page |
1.2.6 conclusion. (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 |
2.5 conclusion. (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 |
3.6 conclusion. (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 |
4.5 conclusion. (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 |
5.3 change in Angular frequency and KS elements. (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 |
5.5 conclusion. (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 |
6.4 conclusion. (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 |
7.5 conclusion. (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 |
8.4 conclusion. (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 |
Table 2-1 - initial condition (position, velocity and osculating orbital parameters). (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 |
Table 8-4: comparison between ANAL and KSANAL values with NUM values of semi-major axis decrease after 500 revolutions with inclination 50 degrees. (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 |
Table 8-5: comparison between ANAL and KSANAL values with NUM values of eccentricity decrease after 500 revolution with inclination 50 degree. (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. 1.2.2: components of the force f?acting on the satellite. (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. 3-1: comparison between ANAL and by 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. 3-2: comparison between ANAL and NUM values of eccentricity decrease alter 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 |
