TITLE: SATELLITE TRAJECTORY MODELLING WITH MISSION TO HALO ORBIT AROUND LAGRANGE POINT 1 (L1) IN THE SUN-EARTH SYSTEM
Since a few decades ago, the Lagrange point had been proposed to be utilized by satellites in carrying out its mission. Missions that utilize the Lagrange point will use the three-body problem where there are two primary objects and one secondary object (satellite). This thesis uses a Circular Restr...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/50051 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |