Full attitude state reconstruction of tumbling space debris TOPEX/Poseidon via light-curve inversion with Quanta Photogrammetry
Autor: | Franz Koidl, Moriba Jah, Georg Kirchner, Michael Steindorfer, James Bennett, D. Kucharski, Peiyuan Wang |
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Rok vydání: | 2021 |
Předmět: |
Physics
020301 aerospace & aeronautics Angular momentum Satellite laser ranging Aerospace Engineering 02 engineering and technology Moment of inertia Geodesy 01 natural sciences 0203 mechanical engineering Position (vector) Orientation (geometry) Physics::Space Physics 0103 physical sciences Satellite 010303 astronomy & astrophysics Reference frame Space debris |
Zdroj: | Acta Astronautica. 187:115-122 |
ISSN: | 0094-5765 |
DOI: | 10.1016/j.actaastro.2021.06.032 |
Popis: | The tumbling motion of defunct satellite TOPEX/Poseidon (T/P) is governed by the μ-scale Solar Radiation Pressure (SRP) torque that spun up the satellite from the initial, nadir-pointing to the current fast spinning state [1]. In this paper, we advance the methods of Quanta Photogrammetry (QPM) in an effort to determine satellite attitude parameters – the inertial orientation of the body angular momentum vector L , the rotational phase and rate as well as the object pole coordinates with respect to L ; the determined pole offset is 3.52°. The presented data support the hypothesis that the full characteristics of the satellite attitude dynamics can be obtained from a single radiant photogram measured by the photon-counting system of the Graz Satellite Laser Ranging (SLR) Observatory during an overhead pass. The analysis of the observed radiant signature of T/P gives the elevation angle of the normal vector to the solar array front surface at −1.7°, RMS = 0.63°, in the spacecraft body-centered reference frame. This information, along with the pole position, is used to model the SRP forces and torques on the satellite and determine the T/P moment of inertia I = 69728 , σ I = 75.2 [ k g m 2 ] , by best-fitting long-term spin simulation to the observed trend. |
Databáze: | OpenAIRE |
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