2019
DOI: 10.1109/jsyst.2019.2919526
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Parametric System Engineering Analysis of Capability-Based Small Satellite Missions

Abstract: To achieve appropriate link budget and system engineering analyses of capability-based small satellites missions, an objective assessment and computation of the component-, subsystem-, and system-levels parameters requirements must be carried out. This paper presents the measurement-derived parametric models for the system engineering analysis of communication, meteorology, planetary, and other small satellite programs with recourse to the initial mission, conceptual design, and postmission objectives. Mass an… Show more

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Cited by 25 publications
(16 citation statements)
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“…The gain shown in Fig. 8 is 40 dB at the band ripple factor across the required end subsystems [30].…”
Section: And Discussionmentioning
confidence: 94%
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“…The gain shown in Fig. 8 is 40 dB at the band ripple factor across the required end subsystems [30].…”
Section: And Discussionmentioning
confidence: 94%
“…receiver sens operating frequency. This appears to justify the choice of the 50 MHz bandwidth for satellite video signals transmission [22], [30] characterization, the allowable temperature drift is ome equipment allow for up to 3 ambient temperature. For any given fabricated MMIC LNA that is characterized, 0.1 to 0.2 dB is the allowable loss margin for linear (S loss of above 1 that there is a need to enhance the receiver sensitivity by performing a component reconfiguration in near real…”
Section: Iv2mentioning
confidence: 99%
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“…The proposed HPDC can be realised within a monolithic microwave integrated circuit (MMIC) low-noise amplifier for adaptive satellite-cellular convergence applications [11], [12]. The novel research findings from the HPDC design holds great promise for advanced capabilitybased reconfigurable R.F transceiver and regenerative satellite transponder frontends [13]- [19]. Moreover, the HPDC is an excellent R.F architecture for hybrid beamformer development for 5G MIMO antenna integration.…”
Section: Introductionmentioning
confidence: 99%
“…A detailed explanation of the factors affecting the link is available in [11]. However, the main challenge for LEO link budgets is not the calculation of the attenuation and atmospheric losses [12], but how to integrate those with the spacecraft mobility over the Earth's surface [13], [14].…”
Section: Introductionmentioning
confidence: 99%