On the tracking strategies and space geometrical relationship between a TDRS and user satellites
YI Ke-chu
Abstract
YI Ke-chu
Abstract
From the viewpoint of tracking strategies and link establishment,this paper studies the space geometrical relationship between a TDRS and user satellites in detail.Taking into account of the occultation caused by the Earth and the body of a satellite,the bidirectional tracking rules for a TDRS and user satellites are investigated based on classical orbital elements and the satellite's attitude.The coverage of a TDRS over a user satellite with different orbital altitudes is calculated and simulated.In order to overcome the occultation caused by the body of a user satellite,a way to fix the antenna to a mast which extrudes above the side towards space of a user satellite is presented.With an appropriate height of the mast,the occultation can be eliminated.All these formulas and strategies are the key elements for TTC and applications of China's future TDRS.
OpenAlex reports 3 citations for this work. Citation counts describe recorded attention and do not establish research quality.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
From the viewpoint of tracking strategies and link establishment,this paper studies the space geometrical relationship between a TDRS and user satellites in detail.Taking into account of the occultation caused by the Earth and the body of a satellite,the bidirectional tracking rules for a TDRS and user satellites are investigated based on classical orbital elements and the satellite's attitude.The coverage of a TDRS over a user satellite with different orbital altitudes is calculated and simulated.In order to overcome the occultation caused by the body of a user satellite,a way to fix the antenna to a mast which extrudes above the side towards space of a user satellite is presented.With an appropriate height of the mast,the occultation can be eliminated.All these formulas and strategies are the key elements for TTC and applications of China's future TDRS.
Key concepts: Satellite, Computer science, Satellite tracking, Tracking (education), Aerospace engineering, Simulation, Engineering, Pedagogy