نویسندگان
دانشگاه صنعتی مالک اشتر
چکیده
کلیدواژهها
عنوان مقاله [English]
نویسندگان [English]
This paper presents simulation results of satellite launch vehicle tracking with Monopulse-Track method.
Monopulse system is Amplitude-Amplitude. In other words, position determination of antenna for satellite
launch vehicle precise tracking with monopulse method is done. Target has maneuvered in the paper and
trajectory changes during the tracking; Consequently probability of error is more than targets such as satellite
that have steady orbit; These targets surveyed in the similar previous works. At the first, we have the data of
supposed trajectory of satellite launch vehicle. The amount of offset of antenna's position with the trajectory is
indicator of prime error antenna tracking which that is the input of monopulse algorithm and the offset is
corrected with the proposed method. Simulation results demonstrate good performance of the proposed method
for satellite launch vehicle tracking.
کلیدواژهها [English]
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