scholarly journals The Simulation and the Calculation of the Shortest Hohmann Transfer Orbit to Mars

2019 ◽  
Vol 07 (10) ◽  
pp. 2384-2400
Author(s):  
Yifan Wei ◽  
Yuke Zhang
2018 ◽  
Author(s):  
Thirugnanasambandan Theivasanthi

Highlights:1) Confirming theoretically by analysing the presence of five elements (Panchaboothams) in Mars and suggests that Mars will be a possible place for life.2) Comparing the analogies between Hohmann transfer orbit concept and our ancients’ astronomical Science knowledge (prior to Hohmann concept). 3) Suggestions based on idea for making spacecraft / satellite into particles and sending them through radio waves and assembled them later.


2021 ◽  
Vol 2 (1) ◽  
Author(s):  
Tao Shi ◽  
Xuebin Zhuang ◽  
Liwei Xie

AbstractThe autonomous navigation of the spacecrafts in High Elliptic Orbit (HEO), Geostationary Earth Orbit (GEO) and Geostationary Transfer Orbit (GTO) based on Global Navigation Satellite System (GNSS) are considered feasible in many studies. With the completion of BeiDou Navigation Satellite System with Global Coverage (BDS-3) in 2020, there are at least 130 satellites providing Position, Navigation, and Timing (PNT) services. In this paper, considering the latest CZ-5(Y3) launch scenario of Shijian-20 GEO spacecraft via Super-Synchronous Transfer Orbit (SSTO) in December 2019, the navigation performance based on the latest BeiDou Navigation Satellite System (BDS), Global Positioning System (GPS), Galileo Navigation Satellite System (Galileo) and GLObal NAvigation Satellite System (GLONASS) satellites in 2020 is evaluated, including the number of visible satellites, carrier to noise ratio, Doppler, and Position Dilution of Precision (PDOP). The simulation results show that the GEO/Inclined Geo-Synchronous Orbit (IGSO) navigation satellites of BDS-3 can effectively increase the number of visible satellites and improve the PDOP in the whole launch process of a typical GEO spacecraft, including SSTO and GEO, especially for the GEO spacecraft on the opposite side of Asia-Pacific region. The navigation performance of high orbit spacecrafts based on multi-GNSSs can be significantly improved by the employment of BDS-3. This provides a feasible solution for autonomous navigation of various high orbit spacecrafts, such as SSTO, MEO, GEO, and even Lunar Transfer Orbit (LTO) for the lunar exploration mission.


2009 ◽  
Vol 65 (7-8) ◽  
pp. 1094-1097 ◽  
Author(s):  
Badaoui El Mabsout ◽  
Osman M. Kamel ◽  
Adel S. Soliman
Keyword(s):  

2014 ◽  
Vol 1049-1050 ◽  
pp. 1803-1807
Author(s):  
Xiao Yang Liu ◽  
Jian Ping Zhao ◽  
Qing Mei Li ◽  
Wei Wang ◽  
Ran Ding ◽  
...  

To adapt to the changing requirement of task data interface under the situation of far distance, multiple segment, multiple circle, multiple satellite and multi-station visibility for satellite misson in transfer orbit segment, the web incremental maintenance system based on materialized view was achieved through applying incremental maintenance principle, database technology, synchronization mechanism and maintenance proxy, and realizing the synchronization and consistency of data interface about the distributed experiment information surveillance software system. The result shows that web incremental maintenance system can ensure the real-time and consistency of data processing and transmission.


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