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2015 |
In-flight performance of the Van Allen Probes RF telecommunications system The NASA Van Allen Probes mission (previously called the Radiation Belt Storm Probes) successfully launched on 30 August 2012. The twin spacecraft, designed, built, and operated by The Johns Hopkins University Applied Physics Laboratory (JHU/APL), has been successfully operating within Earth׳s radiation belts since then, returning critical science data revealing new insights into the physics of the radiation belts. Because of the extreme radiation environment, all spacecraft subsystems including the communications system had to make special accommodations to withstand the effects of the radiation. Each Van Allen Probes spacecraft׳s telecommunications system includes an S-band version of the Frontier Radio, a solid-state power amplifier, RF routing components, and dual low-gain antennas. This mission marks the first flight of the Frontier Radio, which is baselined for use in the upcoming Solar Probe Plus and Europa Clipper missions. This paper will present an overview of the as-built telecommunications system and its ground station interfaces discuss key communications flight hardware components, and then discuss in detail its activities and performance in-flight, including the launch and commissioning operations, performance enhancements since launch, and performance trending in flight. Pre-launch preparations at the APL 18-m ground station revealed occasional RF interference that could disrupt Van Allen Probe downlink. A monitoring system was installed to help mitigate some interference sources, and to characterize the residual environment and show that RF interference was not a mission risk. Post-launch commissioning activities were driven by the requirement to verify both spacecraft׳s communication systems over multiple ground networks, including JHU/APL׳s own 18-m ground station, the Universal Space Network, and TDRSS. Enhanced science data downlink volume was enabled by expanding the usable field of view of the spacecrafts׳ antennas once in-flight calibrations of the antenna patterns were completed, as well as reducing downlink link margins to a bare minimum when downlinking via APL׳s 18-m dish, where the CFDP (CCSDS File Delivery Protocol) is used to guarantee file delivery. Radiation drove some of the hardware design; the radios have experienced several predicted fault conditions at the predicted rates and have reacted autonomously as designed to minimize impact to the science downlink. Srinivasan, Dipak; Adams, Norm; Wallis, Robert; Published by: Acta Astronautica Published on: 11/2015 YEAR: 2015   DOI: 10.1016/j.actaastro.2015.05.001 |
2014 |
Optimization of deep-space Ka-band link schedules Downlink scheduling methods that minimize either contact time or data latency are described. For deep-space missions these two methods yield very different schedules. Optimal scheduling algorithms are straightforward for ideal mission scenarios. In practice, additional schedule requirements preclude a tractable optimal algorithm. In lieu of an optimal solution, an iterative sub-optimal algorithm is described. These methods are motivated in part by a need to balance mission risk, which increases with data latency, and mission cost, which increases with contact time. Cost is reduced by delaying downlink contacts until higher data rates are available. Previous work described optimization of individual Ka-band contacts in the presence of time-varying and statistical link parameters. The present study builds on previous work by using a downlink capacity profile to optimize the downlink schedule over the duration of a mission. The downlink schedule for the NASA mission Solar Probe Plus is used as a case study. Adams, Norman; Copeland, David; Mick, Alan; Pinkine, Nickalaus; Published by: Published on: 03/2014 YEAR: 2014   DOI: 10.1109/AERO.2014.6836351 optimisation; scheduling; space communication links; statistical analysis |
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