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Pith Integrity · Reference Change Desk · events-only

Reference changes

See every place this corpus cites a work that was later retracted, corrected, withdrawn, or placed under expression of concern: exact quote, event source, and what happened next. No model judges the citation.

A notice on this page means a citing paper's bibliography includes a work with a published scholarly-record event. It is not a judgment on the citing paper.

Scoped to citing paper 2501.14173 · clear

01Events with corpus notices

Correction Crossref 1 open · 1 total
Corrigendum to: “Measurement of the <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" altimg="si1.gif" overflow="scroll"> <mml:mi>t</mml:mi> <mml:mover accent="true"> <mml:mrow> <mml:mi>t</mml:mi> </mml:mrow> <mml:mrow> <mml:mo stretchy="false">¯</mml:mo> </mml:mrow> </mml:mover> </mml:math> production cross-section using eμ events with b-tagged jets in pp collisions at <mml:math xmlns:mml="http://www.w3.org/1998/Math/MathML" altimg="si2.gif" overflow="scroll"> <mml:msqrt> <mml:mi>s</mml:mi> </mml:msqrt> <mml:mo>=</mml:mo> <mml:mn>13</mml:mn> </mml:math>  TeV with the ATLAS detector” [Phys. Lett. B 761 (2016) 136–157]

DOI 10.1016/j.physletb.2016.08.019 · event 2017-09-21 · event page · JSON

02One-hop citation notices (secondary index)

Correction Crossref Open
Constrained Fuel and Time Optimal 6DOF Powered Descent Guidance Using Indirect Optimization

cites Path Constraint Regularization in Optimal Control Problems using Saturation Functions, · ref [36] · event 2018-01-26 · 2501.14173 · event page · DOI 10.2514/6.2018-0018

Raw extraction · citation context

50, No. 1, 2017, pp. 4070-4075. https://doi.org/10.1016/j.ifacol.2017.08.790. [36] Antony, T., and Grant, M. J., "Path Constraint Regularization in Optimal Control Problems using Saturation Functions,"2018 AIAA Atmospheric Flight Mechanics Conference, American Institute of Aeronautics and Astronautics, Kissimmee, Florida, 2018, p. 10. https://doi.org/10.2514/6.2018-0018. [37] Epenoy, R., "Fuel Optimization for Continuous-Thrust Orbital Rendezvous with Collision Avoidance Cons…