Cited by 339Spacecraft Design and TechnologySpace Technology and ApplicationsSpace Satellite Systems and Control

Survey of worldwide pico- and nanosatellite missions, distributions and subsystem technology

Bouwmeester, J., Guo, J.·2010·Acta Astronautica

Integrity signals

Registry

Crossref · 10.1016/j.actaastro.2010.06.004

Cites

Statistics

Recomputing p-values needs the paper’s full text.

Claims the paper makes

We couldn’t retrieve this paper’s full text, so its claims and self-check weren’t run. The registry and citation checks still apply.

Claims other papers make about this one

Each is checked against this paper’s own text: does it say what the citing paper says it does?

  • The MPPT-based architecture forces the solar array output voltage to be always set at the value which results in maximum power transfer from the array to the aggregated load, regardless of solar cell temperature and degradation degree.

    “To overcome this limitation, the MPPT-based architecture is proposed [37], which essentially forces the solar array output voltage to be always set at the value which results in the maximum power transfer from the array to the aggregated load, regardless of the solar cell temperature and degradation degree.”

    From A Comprehensive Review on Small Satellite Microgrids (2022) · cites this paper as [37]

The citation lists haven’t been fetched yet

References 9 · Cited by 339

Authors
Bouwmeester, J., & Guo, J.
Affiliations
Delft University of Technology (NL)
Corresponding author
Guo, J.
Venue
Acta Astronautica
Publisher
Elsevier BV
Published
2010-10
Volume
67
Issue
7-8
Pages
854-862
ISSN
0094-5765 (ISSN-L)
OpenAlex
W2118203476
Cited by
339
References
9
Citations by year
2026: 14 · 2025: 20 · 2024: 17 · 2023: 16 · 2022: 21 · 2021: 19 · 2020: 43 · 2019: 29 · 2018: 33 · 2017: 28 · 2016: 25 · 2015: 22 · 2014: 24 · 2013: 17 · 2012: 9
FWCI
17.61
Type
journal article
Language
en
Open access
closed
Locations
Acta Astronautica (publishedVersion)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
  • Physical Sciences › Engineering › Electrical and Electronic Engineering › Space Technology and Applications
  • Physical Sciences › Engineering › Aerospace Engineering › Space Satellite Systems and Control
Keywords
picosatellites, nanosatellites, CubeSat, small satellite mission, attitude control system, technology demonstration, low-cost satellite development

About these checks

Registry, retraction, Cites and statistics results are computed, not judged, with one exception: a printed reference that no index lists is read once by a model before it counts as a citation error. Claims are extracted by a model and kept only when their quote appears verbatim in the text; each cited source is then checked, with a model’s help, for whether it says what the claim relies on. Those verdicts can be wrong — read the claim’s quote and the cited source before relying on one.

Statistics and arithmetic are recomputed, not judged.

Confidence bands are shown only for fields calibrated on our annotated test set. None is calibrated yet, so no band is shown.

What counts as a claim ›How we measure confidence ›How we check this ›

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