Adaptive radiation- and plasma-resilient power electronics for deep-space applications
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.
Anahtar Kelimeler
Tam Kayıt
| Alan | Değer | Dil |
|---|---|---|
| dc.contributor.author | Can, Erol | |
| dc.date.accessioned | 2026-10-18T20:25:25.694716010Z | |
| dc.date.available | 2026-10-18T20:25:25.694716010Z | |
| dc.date.issued | 2026 | |
| dc.description.abstract | 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. | |
| dc.identifier.doi | 10.1080/10420150.2026.2721515 | |
| dc.identifier.eissn | 1029-4953 | |
| dc.identifier.issn | 1042-0150 | |
| dc.identifier.scopus | 2-s2.0-105049929288 | |
| dc.identifier.uri | https://rdlopen.rawdatalibrary.net/r/ebyu/10168 | |
| dc.identifier.wos | WOS:001865284800001 | |
| dc.language.iso | en | |
| dc.publisher | Taylor and Francis Ltd. | |
| dc.relation.ispartof | Radiation Effects and Defects in Solids | |
| dc.rights | info:eu-repo/semantics/openAccess | |
| dc.subject | adaptive control | |
| dc.subject | DC–DC converter | |
| dc.subject | MRAC | |
| dc.subject | radiation-hardened electronics | |
| dc.subject | single-event upset (SEU) | |
| dc.subject | Space plasma | |
| dc.subject | space power systems | |
| dc.subject | DC-DC converters | |
| dc.subject | Electric charge | |
| dc.subject | Electrostatic devices | |
| dc.subject | Electrostatic discharge | |
| dc.subject | Hardening | |
| dc.subject | Interplanetary flight | |
| dc.subject | Plasma diagnostics | |
| dc.subject | Plasma stability | |
| dc.subject | Power quality | |
| dc.subject | Radiation hardening | |
| dc.subject | Radiation shielding | |
| dc.subject | Solar wind | |
| dc.subject | Space applications | |
| dc.subject | Spacecraft power supplies | |
| dc.subject | Topology | |
| dc.subject | Transient analysis | |
| dc.subject | DC converter | |
| dc.subject | Model-reference adaptive controls | |
| dc.subject | Plasma-induced | |
| dc.subject | Radiation hardened electronics | |
| dc.subject | Single event upsets | |
| dc.subject | Single-event upset | |
| dc.subject | Space environment | |
| dc.title | Adaptive radiation- and plasma-resilient power electronics for deep-space applications | |
| dc.type | Article | |
| dspace.entity.type | Publication | |
| rdl.citation.scopus | 0 | |
| rdl.citation.wos | 0 | |
| rdl.source.index | SCOPUS | |
| rdl.source.index | WOS | |
| rdl.wos.index | Science Citation Index Expanded (SCI-EXPANDED) |
