Open AccessSatellite Orbit Design and Analysis Based on STK
Author(s) -
Shilin Zhang
Publication year - 2022
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/2228/1/012037
Subject(s) - satellite , orbit (dynamics) , computer science , simulated annealing , aerospace , low earth orbit , set (abstract data type) , aerospace engineering , orbital elements , algorithm , engineering , physics , astronomy , programming language
The design and analysis of satellite orbits has always been a hot topic in the aerospace field. Through the selection and optimization of orbital parameters, the satellite can meet the corresponding performance indicators and work requirements. However, there are often various constraints in actual scenes, so the orbital parameters cannot be set arbitrarily. Therefore, how to design the orbit under the constraints to make the satellite in optimum condition is very important. Based on STK, this paper proposes a satellite orbit design method, and realizes the optimization of the orbit through the simulated annealing algorithm. The simulation results show that this method can achieve satisfactory results and has certain practical value.