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The Use of the GNSS Technologies to Determine the Parameters of a Lander’s Trajectory During the Atmospheric Phase of Its Motion

V. S. Vasilev, М. A. Voronov, А. S. Bikov, S. U. Medvedev, B. A. Sakharov

Transactions of IAA RAS, issue 43, 36–41 (2017)

Keywords: point of reception of telemetry and ranging signals, control, positioning and timing support, instrument for time and frequency synchronization, navigation parameters, movement parameters

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Abstract

It is known that the motion of landers in the atmosphere with velocities exceeding a few km/s is accompanied by the appearance of the edge plasma of ionized and turbulent flows in the base region. Reception of the GNSS signals on board becomes impossible for the descent apparatus under these conditions after it reaches a certain height. However, it is difficult to imagine a modern trajectory measuring system (including for this kind of flight conditions) to be created without the use of the GNSS technologies. We define the parameters of the lander’s trajectory during the atmospheric phase of its movement using the GNSS technologies and signals emitted by the onboard telemetry system.

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V. S. Vasilev, М. A. Voronov, А. S. Bikov, S. U. Medvedev, B. A. Sakharov. The Use of the GNSS Technologies to Determine the Parameters of a Lander’s Trajectory During the Atmospheric Phase of Its Motion // Transactions of IAA RAS. — 2017. — Issue 43. — P. 36–41. @article{vasilev2017, abstract = {It is known that the motion of landers in the atmosphere with velocities exceeding a few km/s is accompanied by the appearance of the edge plasma of ionized and turbulent flows in the base region. Reception of the GNSS signals on board becomes impossible for the descent apparatus under these conditions after it reaches a certain height. However, it is difficult to imagine a modern trajectory measuring system (including for this kind of flight conditions) to be created without the use of the GNSS technologies. We define the parameters of the lander’s trajectory during the atmospheric phase of its movement using the GNSS technologies and signals emitted by the onboard telemetry system.}, author = {V.~S. Vasilev and М.~A. Voronov and А.~S. Bikov and S.~U. Medvedev and B.~A. Sakharov}, issue = {43}, journal = {Transactions of IAA RAS}, keyword = {point of reception of telemetry and ranging signals, control, positioning and timing support, instrument for time and frequency synchronization, navigation parameters, movement parameters}, pages = {36--41}, title = {The Use of the GNSS Technologies to Determine the Parameters of a Lander’s Trajectory During the Atmospheric Phase of Its Motion}, url = {http://iaaras.ru/en/library/paper/1762/}, year = {2017} } TY - JOUR TI - The Use of the GNSS Technologies to Determine the Parameters of a Lander’s Trajectory During the Atmospheric Phase of Its Motion AU - Vasilev, V. S. AU - Voronov, М. A. AU - Bikov, А. S. AU - Medvedev, S. U. AU - Sakharov, B. A. PY - 2017 T2 - Transactions of IAA RAS IS - 43 SP - 36 AB - It is known that the motion of landers in the atmosphere with velocities exceeding a few km/s is accompanied by the appearance of the edge plasma of ionized and turbulent flows in the base region. Reception of the GNSS signals on board becomes impossible for the descent apparatus under these conditions after it reaches a certain height. However, it is difficult to imagine a modern trajectory measuring system (including for this kind of flight conditions) to be created without the use of the GNSS technologies. We define the parameters of the lander’s trajectory during the atmospheric phase of its movement using the GNSS technologies and signals emitted by the onboard telemetry system. UR - http://iaaras.ru/en/library/paper/1762/ ER -