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Record W2923887854 · doi:10.2514/1.g003445

Attitude Stabilization Using Two Parallel Single-Gimbal Control Moment Gyroscopes

2019· article· en· W2923887854 on OpenAlex

Why this work is in the frame

A frame that forgets how it found something cannot be audited. These are the routes that admitted this work.

affAt least one author lists a Canadian institution in the pinned OpenAlex snapshot.

Bibliographic record

VenueJournal of Guidance Control and Dynamics · 2019
Typearticle
Languageen
FieldEngineering
TopicMagnetic Bearings and Levitation Dynamics
Canadian institutionsToronto Metropolitan University
Fundersnot available
KeywordsControl moment gyroscopeUnderactuationControl theory (sociology)Angular momentumAttitude controlGimbalGyroscopeSpacecraftControllabilityPhysicsReaction wheelMoment (physics)Controller (irrigation)TorqueTotal angular momentum quantum numberComputer scienceEngineeringMathematicsClassical mechanicsAerospace engineeringNonlinear systemControl (management)

Abstract

fetched live from OpenAlex

This paper investigates the underactuated attitude stabilization problem using two parallel single-gimbal control moment gyroscopes (SGCMGs). Different from most existing underactuated control techniques requiring the zero total angular momentum assumption, only the controllability of the whole control moment gyroscope (CMG)–spacecraft system, which means the total angular momentum of the spacecraft with CMG array within the momentum envelope of the CMG array, is required in this paper. To achieve the underactuated attitude stabilization, a new controller consisting of two parts, that is, a higher level sliding mode control part to stabilize the angular velocity about the underactuated axis in finite time and a tracking control part to track desired angular velocities that are used to stabilize the remaining states, is developed. This proposed novel control logic achieves attitude stabilization when the initial total angular momentum of the CMG-spacecraft is not zero. Simulations show that the attitude of a microsatellite can be stabilized precisely within acceptable time using the proposed control law and steering law when the controllability constraint is satisfied. When the initial total momentum of the spacecraft base and the CMG array exceeds the momentum envelope of the CMG array, simulation results demonstrate that the attitude is controlled to be a periodic oscillation in the vicinity of the equilibrium, at the same angular momentum level determined by the initial condition.

Fetched live from OpenAlex and de-inverted. Abstracts are not stored in this database: the inverted indexes are 8.6 GB of the frame’s 9.3 GB of text, and the host has 13 GB free.

Full frame distilled prediction

Teacher imitation

Not calibrated prevalence, not ground truth. Human validation pending. Learned from the 10,348 direct Codex labels and 10,348 direct Gemma labels. Candidate is the union of thresholded teacher heads; consensus is their intersection. These outputs are machine_predicted_unvalidated and are not human labels or direct frontier model labels.

metaresearch head score (Codex)0.000
metaresearch head score (Gemma)0.000
Version: codex-gemma-dda1882f352aValidation status: machine_predicted_unvalidated
Candidate categoriesnone
Consensus categoriesnone
DomainCandidate signal: none · Consensus signal: none
Study designCandidate signal: Simulation or modeling · Consensus signal: Simulation or modeling
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.447
Threshold uncertainty score0.606

Codex and Gemma teacher scores by category

CategoryCodexGemma
Metaresearch0.0000.000
Meta-epidemiology (narrow)0.0000.000
Meta-epidemiology (broad)0.0000.000
Bibliometrics0.0000.000
Science and technology studies0.0000.000
Scholarly communication0.0000.000
Open science0.0000.000
Research integrity0.0000.000
Insufficient payload (model declined to judge)0.0000.000

Machine scores (provisional)

The two teacher heads of the student model, read on this work. A score orders the frame for review; it never asserts a category, and the validation status ships verbatim with every row.

Baseline scores from an immature model (maturity gate not passed, 7 training rounds). Scores rank; they never assert a category.

Opus teacher head0.007
GPT teacher head0.217
Teacher spread0.210 · how far apart the two teachers sit on this one work
Validation statusscore_only:v0-immature-baseline · verbatim from the scoring run: score_only means the number may rank works, and no category label ships from it