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Record W7132442261

Missile propulsion performance modeling in a visual simulation environment

2001· article· en· W7132442261 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

VenueTNO Repository · 2001
Typearticle
Languageen
FieldEngineering
TopicGuidance and Control Systems
Canadian institutionsnot available
Fundersnot available
KeywordsMissilePropulsionComponent (thermodynamics)Weapon systemRocket (weapon)FidelityPropellantHigh fidelityModeling and simulation
DOInot available

Abstract

fetched live from OpenAlex

The Defence Research Establishment Valcartier (DREV) in Canada and the TNO Prins Maurits Laboratory (TNO-PML) in the Netherlands are investigating ducted rocket propulsion technology and its impact on missile performance in a collaborative research program. One key component of this collaboration is the development of a Modeling and Simulation (M&S) capability to evaluate the applicability, benefits and limitations of the ducted rocket for air-to-air missiles in realistic mission engagement scenarios. Since the engagement simulation is used specifically to assess the impact of missile propulsion on overall weapon performance, the selection of the components of the missile model and their level of fidelity have been purposely tailored to focus on those performance drivers having a dependence on the propulsion system.The engagement model includes a six-degree-of-freedom (6DOF) representation of the missile flight dynamics as well as component models of suitable fidelity for the seeker, guidance and autopilot. The core component of the missile model is the standalone Fortran-based TNO DREV ducted rocket engine model. The complete engagement model including the launcher aircraft, missile and target, was implemented in Matlab/Simulink to take advantage of the wide range of features available. Visual environments provide an integrated capability for fast prototyping of dynamic systems, facilitate team development through a standard approach for model implementation, and offer a flexible mechanism for the re-use of legacy models. Sample results of simulated missile-target engagements illustrate the application of this simulation capability to missile propulsion trade-off studies and analysis of system concepts.

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 score0.033
Threshold uncertainty score0.313

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 head0.011
GPT teacher head0.200
Teacher spread0.189 · 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