Adaptive radiation- and plasma-resilient power electronics for deep-space applications

ArticleAçık Erişim

Özet

Space missions expose spacecraft electronics to complex space environments, including charged particle fluxes, solar wind plasma, and high-energy radiation, which can induce surface charging, electrostatic discharges (ESD), and single-event upsets (SEUs) in power conversion systems. Traditional mitigation strategies, such as radiation-hardened components and shielding, offer partial protection but incur significant mass and efficiency penalties and do not address transient plasma-induced disturbances. This study presents a physics-informed, plasma-resilient design methodology for DC–DC converters in deep-space applications. A comprehensive space-environment simulation framework is developed to model heliocentric plasma density, solar wind velocity, proton energy spectra, and surface charging, incorporating both low- and high-frequency fluctuations. Building on this, a radiation-aware, adaptive DC–DC converter topology is proposed, coupled with a model reference adaptive control (MRAC) architecture and disturbance observer, enabling real-time mitigation of plasma-induced voltage fluctuations, SEU step events, and input ripple. Simulation results demonstrate that the proposed approach maintains the output voltage close to the nominal value under the considered space-environment disturbances. The adaptive controller reduces the RMS voltage error from approximately 10.3–12.6 V in the uncontrolled system to approximately 1.86–1.91 V across the investigated operating scenarios while significantly suppressing transient deviations caused by plasma fluctuations and SEU events. Frequency-domain analysis confirms effective attenuation of low-frequency plasma-induced transients, while Lyapunov-based stability proofs ensure guaranteed closed-loop robustness. The integrated methodology enables reliable, efficient, and adaptive energy management for long-duration space missions, highlighting the importance of environment-aware hardware-control co-design for future deep-space spacecraft. © 2026 Informa UK Limited, trading as Taylor & Francis Group.

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AlanDeğerDil
dc.contributor.authorCan, Erol
dc.date.accessioned2026-10-18T20:25:25.694716010Z
dc.date.available2026-10-18T20:25:25.694716010Z
dc.date.issued2026
dc.description.abstractSpace missions expose spacecraft electronics to complex space environments, including charged particle fluxes, solar wind plasma, and high-energy radiation, which can induce surface charging, electrostatic discharges (ESD), and single-event upsets (SEUs) in power conversion systems. Traditional mitigation strategies, such as radiation-hardened components and shielding, offer partial protection but incur significant mass and efficiency penalties and do not address transient plasma-induced disturbances. This study presents a physics-informed, plasma-resilient design methodology for DC–DC converters in deep-space applications. A comprehensive space-environment simulation framework is developed to model heliocentric plasma density, solar wind velocity, proton energy spectra, and surface charging, incorporating both low- and high-frequency fluctuations. Building on this, a radiation-aware, adaptive DC–DC converter topology is proposed, coupled with a model reference adaptive control (MRAC) architecture and disturbance observer, enabling real-time mitigation of plasma-induced voltage fluctuations, SEU step events, and input ripple. Simulation results demonstrate that the proposed approach maintains the output voltage close to the nominal value under the considered space-environment disturbances. The adaptive controller reduces the RMS voltage error from approximately 10.3–12.6 V in the uncontrolled system to approximately 1.86–1.91 V across the investigated operating scenarios while significantly suppressing transient deviations caused by plasma fluctuations and SEU events. Frequency-domain analysis confirms effective attenuation of low-frequency plasma-induced transients, while Lyapunov-based stability proofs ensure guaranteed closed-loop robustness. The integrated methodology enables reliable, efficient, and adaptive energy management for long-duration space missions, highlighting the importance of environment-aware hardware-control co-design for future deep-space spacecraft. © 2026 Informa UK Limited, trading as Taylor & Francis Group.
dc.identifier.doi10.1080/10420150.2026.2721515
dc.identifier.eissn1029-4953
dc.identifier.issn1042-0150
dc.identifier.scopus2-s2.0-105049929288
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/ebyu/10168
dc.identifier.wosWOS:001865284800001
dc.language.isoen
dc.publisherTaylor and Francis Ltd.
dc.relation.ispartofRadiation Effects and Defects in Solids
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectadaptive control
dc.subjectDC–DC converter
dc.subjectMRAC
dc.subjectradiation-hardened electronics
dc.subjectsingle-event upset (SEU)
dc.subjectSpace plasma
dc.subjectspace power systems
dc.subjectDC-DC converters
dc.subjectElectric charge
dc.subjectElectrostatic devices
dc.subjectElectrostatic discharge
dc.subjectHardening
dc.subjectInterplanetary flight
dc.subjectPlasma diagnostics
dc.subjectPlasma stability
dc.subjectPower quality
dc.subjectRadiation hardening
dc.subjectRadiation shielding
dc.subjectSolar wind
dc.subjectSpace applications
dc.subjectSpacecraft power supplies
dc.subjectTopology
dc.subjectTransient analysis
dc.subjectDC converter
dc.subjectModel-reference adaptive controls
dc.subjectPlasma-induced
dc.subjectRadiation hardened electronics
dc.subjectSingle event upsets
dc.subjectSingle-event upset
dc.subjectSpace environment
dc.titleAdaptive radiation- and plasma-resilient power electronics for deep-space applications
dc.typeArticle
dspace.entity.typePublication
rdl.citation.scopus0
rdl.citation.wos0
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)