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Hyperspectral Lightcurve Inversion for Attitude Determination
Signal Processing · Submitted 19 Dec 2023
abstract compiled · 2026-09-23 · no language-model review
The authors' main claim Results are shown based on synthetic data.
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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.
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The abstract, sentence by sentence
Spectral lightcurves consisting of time series single-pixel spectral measurements of spacecraft are used to infer the spacecraft's attitude and rotation. Two methods are used. One based on numerical optimisation of a regularised least squares cost function, and another based on machine learning with a neural network model. The aim is to work with minimal information, thus no prior is available on the attitude nor on the inertia tensor. The theoretical and practical aspects of this task are investigated, and the methodology is tested on synthetic data. Results are shown based on synthetic data.
background contribution method result interpretation main claim
| # | sentence | role | the authors' own work | states the main conclusion | strength |
|---|---|---|---|---|---|
| s0 | Spectral lightcurves consisting of time series single-pixel spectral measurements of spacecraft are used to infer the spacecraft's attitude and rotation. Two methods are used. | background 0.40 | 0.49 | 0.04 | asserted 1.00 |
| s1 | One based on numerical optimisation of a regularised least squares cost function, and another based on machine learning with a neural network model. | method 0.99 | 0.68 | 0.04 | asserted 0.94 |
| s2 | The aim is to work with minimal information, thus no prior is available on the attitude nor on the inertia tensor. | background 0.51 | 0.35 | 0.04 | asserted 0.98 |
| s3 | The theoretical and practical aspects of this task are investigated, and the methodology is tested on synthetic data. | contribution 0.74 | 0.85 | 0.04 | asserted 0.98 |
| s4 | Results are shown based on synthetic data. | result 0.89 | 0.89 | 0.09 | asserted 0.98 |
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The paper
Original abstract
Spectral lightcurves consisting of time series single-pixel spectral measurements of spacecraft are used to infer the spacecraft's attitude and rotation. Two methods are used. One based on numerical optimisation of a regularised least squares cost function, and another based on machine learning with a neural network model. The aim is to work with minimal information, thus no prior is available on the attitude nor on the inertia tensor. The theoretical and practical aspects of this task are investigated, and the methodology is tested on synthetic data. Results are shown based on synthetic data.
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The training is done using the Adam optimiser [ref] , with the mean squared error (MSE) loss function.
Adam: A Method for Stochastic Optimization · Network Architecture · 1.00
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