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Record W1663088614

Validation of Innovative State Estimation and Control Techniques on PROBA-2

2006· article· en· W1663088614 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.

aboutThe title or abstract carries a Canadian signal from the geographic lexicon.
no affNo Canadian affiliation: this work is invisible to an affiliation-only frame.
No Canadian affiliation. An affiliation-only frame, the usual design, would never have seen this work. It is one of the works that make the case for inverting the frame.

Bibliographic record

VenueESASP · 2006
Typearticle
Languageen
FieldEngineering
TopicInertial Sensor and Navigation
Canadian institutionsnot available
Fundersnot available
KeywordsSpacecraftAutonomyComputer scienceAttitude controlOrbit determinationSatelliteSpace technologyOrbit (dynamics)Aerospace engineeringInternational Space StationSystems engineeringEngineeringPolitical science
DOInot available

Abstract

fetched live from OpenAlex

ABSTRACT PROBA-2 is an ESA technology-demonstration mission aimed at the demonstration of autonomy-enabling space technologies. This paper will describe the PROBA-2 mission, the Attitude and Orbit Control System (AOCS) software and its new features compared to its predecessor, PROBA-1. The simulations presented will also demonstrate some of the new estimation and control techniques to be validated on PROBA-2, including attitude and orbit determination using temperature, light and/or magnetic-field sensors, attitude and orbit estimation using a Square-Root Unscented Kalman Filter and the high-precision execution of large-angle maneuvers with a constrained rotation axis. 1 INTRODUCTION Although the on-board autonomy of spacecraft has already been demonstrated, its interest still remains for the international scientific community. Autonomy refers to the migration of intelligence and decision capability from the ground station to the spacecraft. The PRoject for On-Board Autonomy program (PROBA), sponsored by European Space Agency (ESA), aims at the demonstration of on-board autonomy-enabling technologies with the objectives of reducing mission-operation costs and maximizing the efficiency of spacecraft operation. The development of on-board autonomy has the potential benefits of better managing the limited on-board resources and reducing the ground station operating costs. In addition, it could benefit to future interplanetary missions where there is no Earth contact for extended duration. PROBA-2 is the second in-orbit demonstration mini-satellite developed by ESA. Following the success of PROBA-1, PROBA-2 will continue the in-flight demonstration of onboard-autonomy technologies while maintaining low development costs. PROBA-2 is an agile mini-satellite currently under development by Verhaert Space (Belgium), the Prime Contractor, supported by Spacebel informatique (Belgium) and NGC Aerospace Ltd (Canada). The launch is foreseen in early 2007. In order to fully demonstrate the technology in a real mission scenario, various payloads will be flown on PROBA-2 to exercise and validate the advanced autonomy capabilities of the spacecraft through a Sun-observation and space plasma mission. Following a brief description of the PROBA-2 mission, spacecraft and Attitude and Orbit Control System (AOCS) hardware, this paper will present the AOCS on-board software, and particularly, its new features compared to PROBA-1: large-angle rotation along a constrained axis, Earth avoidance detection and pseudo-measurements to deal with single-vector measurements. The paper will also present a progress report on new autonomy-enabling AOCS techniques, proposed by NGC Aerospace, to be validated in flight. These include the use of a Square-Root Unscented Kalman Filter (SRUKF) for attitude and orbit determination, the validation of a low-cost orbit determination based on temperature sensor and a magnetic-only orbit and attitude navigation system.

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: Bench or experimental · Consensus signal: Bench or experimental
GenreCandidate signal: Empirical · Consensus signal: Empirical
Teacher disagreement score0.136
Threshold uncertainty score0.174

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 head0.003
GPT teacher head0.203
Teacher spread0.200 · 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