Pith. Sign in

RECORD

Suppression of Chaotic Motion of Tethered Satellite Systems Using Tether Length Control

PaperPDF from arXiv

data files

Paper breakdownThe authors' claims, conditions and measurements, as JSON Signed receiptProof this review has not been altered
X Bluesky LinkedIn Reddit Hacker News
Francisco J. T. Salazar, Antonio F. B. A. Prado

Earth and Planetary Astrophysics · Submitted 25 Jul 2023

abstract compiled · 2026-09-23 · no language-model review

The authors' main claim This study focuses on attitude and control motion of two bodies (a base-satellite and a sub-satellite) connected by an inextensible and massless tether in a circular orbit under the influence of the Earths gravitational force.

how it is stated · asserted 0.95 read the record →

Comment (0) Read on arXiv ↗
Cite ▾
arXiv ID2307.12990 (version 1)
Pith ID6VGJGLDN, Pith's permanent record of this paper and its review
CitationAntonio F. B. A. Prado, Francisco J. T. Salazar. "Suppression of Chaotic Motion of Tethered Satellite Systems Using Tether Length Control." arXiv:2307.12990 (2023). https://pith.science/paper/6VGJGLDN
Claim paper

The compiled record

The paper's own sentences, arranged. Each label is drawn from a closed vocabulary; the number beside it is the probability the classifier gave that label. Numbers in the tables are the authors', checked by code. No sentence in this record was written by a model.

Open the compiled record

Compiled by classifier-1.13.0 via TypeSafe API, question bank abstract-p1-20260923, 2026-09-23: 1 request, 3,645 input tokens.

What the abstract itself states, as probabilities: claims first 0.02 · states limitation 0.93 · human participants 0.01 · controlled comparison 0.04 · randomized assignment 0.01 · states quantitative result 0.03 · compares with prior results 0.04 · mentions code or data availability 0.02.

The abstract, sentence by sentence

arXiv listing abstract v1. Results and the main claim are underlined; .

This study focuses on attitude and control motion of two bodies (a base-satellite and a sub-satellite) connected by an inextensible and massless tether in a circular orbit under the influence of the Earths gravitational force. The base-satellite is assumed to be far more heavier than the sub-satellite. In such cases, the base-satellite is regarded as the reference spacecraft. Because of the complexity of the problem, no thrusters on the sub-satellite are considered, and the effect of atmospheric drag, Earths oblateness, and electrodynamic force on the spacecraft are neglected.

background contribution method result interpretation main claim

What the classifier reports for each sentence. The number is the probability it gave the label.
#sentencerolethe authors' own workstates the main conclusionstrength
s0 This study focuses on attitude and control motion of two bodies (a base-satellite and a sub-satellite) connected by an inextensible and massless tether in a circular orbit under the influence of the Earths gravitational force. contribution 0.50 0.27 0.03 asserted 0.95
s1 The base-satellite is assumed to be far more heavier than the sub-satellite. background 0.56 0.17 0.02 asserted 0.99
s2 In such cases, the base-satellite is regarded as the reference spacecraft. background 0.74 0.21 0.02 asserted 0.99
s3 Because of the complexity of the problem, no thrusters on the sub-satellite are considered, and the effect of atmospheric drag, Earths oblateness, and electrodynamic force on the spacecraft are neglected. limitation 0.80 0.47 0.02 asserted 0.99

What kind of paper the classifier reports this is: method or tool 0.85 · evidence from simulation or computation 0.42.

What was examined, and what was not

sources read
  • arXiv listing abstract v1
not examined
  • full text
  • figures and tables
  • references and citing sentences
  • relations to other papers
levels run
  • P abstract
not run
  • S sections
  • T body sentences
  • C citations
  • R cross-paper relations

Every quoted sentence on this record is the authors'. Every label is from Pith's closed vocabulary, with the probability shown beside it. Every number in the measurements table is the authors', checked by code. Record as JSON

The paper
Original abstract

This study focuses on attitude and control motion of two bodies (a base-satellite and a sub-satellite) connected by an inextensible and massless tether in a circular orbit under the influence of the Earths gravitational force. The base-satellite is assumed to be far more heavier than the sub-satellite. In such cases, the base-satellite is regarded as the reference spacecraft. Because of the complexity of the problem, no thrusters on the sub-satellite are considered, and the effect of atmospheric drag, Earths oblateness, and electrodynamic force on the spacecraft are neglected.

Human review

How Pith checks papers → · Full audit of this paper →

Discussion

Know something about this paper? Leave a comment, or highlight any passage above to comment on it.