
This paper introduced the adoption of a Track Sensor on the satellite of the STSS to improve the precision of the STSS. The concepts of space coverage were proposed and the corresponding models established. A simplified computation strategy of space coverage was proposed to obtain the simulation results. Space coverage rate under different scenarios was simulated as well as its characteristics illustrated. Finally, a valuable result about the optimal orbit altitude for the given working distance of the Track Sensor regardless of the specific constellation was obtained.
surveillance systems, satellite tracking, ResPubID20788, attitude control, computational modelling, orbits, School of Law, earth, performance evaluation, optimal orbit altitude, space tracking, missiles, 0102 Applied Mathematics, 1005 Communications Technologies, 970101 Expanding Knowledge in the Mathematical Sciences, chromium, performance analysis, position control, mathematical models, track sensor location
surveillance systems, satellite tracking, ResPubID20788, attitude control, computational modelling, orbits, School of Law, earth, performance evaluation, optimal orbit altitude, space tracking, missiles, 0102 Applied Mathematics, 1005 Communications Technologies, 970101 Expanding Knowledge in the Mathematical Sciences, chromium, performance analysis, position control, mathematical models, track sensor location
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