2006 IEEE Aerospace Conference
DOI: 10.1109/aero.2006.1655857
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Telemetry Recovery and Uplink Commanding of a Spacecraft Prior to Three-Axis Attitude Stabilization

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Cited by 4 publications
(5 citation statements)
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“…For example, before the attitude stabilization or at the end of mission due to a fail of attitude control system, the satellite could casually lose stability. In this scenario, the channel results to be very un-stable and the signal strength would follow the antenna radiation pattern dropping out completely when the antenna rotates away from ground station [10]. Fig.…”
Section: A Scenariomentioning
confidence: 96%
“…For example, before the attitude stabilization or at the end of mission due to a fail of attitude control system, the satellite could casually lose stability. In this scenario, the channel results to be very un-stable and the signal strength would follow the antenna radiation pattern dropping out completely when the antenna rotates away from ground station [10]. Fig.…”
Section: A Scenariomentioning
confidence: 96%
“…Figure 1A reports the SNR values at the receiver as a function of time during a visibility window; its minimum values are reached at the beginning and at the end of each window, ie, when the satellite is close to the horizon. On the other hand, Figure 1B shows the SNR versus time in case of uncontrolled attitude of the spacecraft; the signal strength presents large variations because of satellite motion …”
Section: Scenariomentioning
confidence: 99%
“…The early operations after separation from upper launcher stages, as well as the end of life disposal manoeuvres, are critical satellite mission phases that require a robust and reliable communication system . In these scenarios, the spacecraft may have reduced functionalities and uncontrolled attitude, and consequently, the communication link could be weak and unstable, eg, signal's amplitude may be subjected to deep fading according to satellite tumbling rate . In this context, the communication becomes bursty and the link reliability harms the bit‐rate performance.…”
Section: Introductionmentioning
confidence: 99%
“…The minimum E b /N 0 14 dB is in the downlink curve at the beginning and end of each visibility window, when the satellite is closer to the horizon. Nevertheless, in a scenario with damaged attitude control system, the channel results becomes extremely unstable and the signal strength would follow the antenna radiation pattern dropping out completely when the antenna rotates away from ground station [6]. Figure 3 reports the values of the previously considered curves as given by the link budget curves in a possible critical scenario.…”
Section: Link-budgetmentioning
confidence: 99%
“…The reliability and robustness are key features for a satellite communication system, particularly during critical satellite mission phases, like the early operations after separation from upper launcher stages or the end of life manoeuvres [3,4]. In these scenarios, the spacecraft may have reduced functionalities and uncontrolled attitude and consequently, the communication link could be weak, unstable and with a rapid variability e.g., signal's amplitude could drop down or go up according to satellite tumbling rate [5,6]. In this context, the communication becomes bursty and the link reliability harms the bit rate performance.…”
Section: Introductionmentioning
confidence: 99%