Projection-Based Reduced-Order Modeling for Spacecraft Thermal Analysis

This paper presents a mathematically rigorous, subspace projection-based reduced-order modeling methodology and an integrated framework to automatically generate reduced-order models for spacecraft thermal analysis. Two key steps in the reduced-order modeling procedure are described: first, the acqu...

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Veröffentlicht in:	Journal of spacecraft and rockets 2015-05, Vol.52 (3), p.978-989
Hauptverfasser:	Qian, Jing, Wang, Yi, Song, Hongjun, Pant, Kapil, Peabody, Hume, Ku, Jentung, Butler, Charles D
Format:	Artikel
Sprache:	eng
Schlagworte:	Acceleration Algebra Computation Differential equations Empirical analysis Error analysis Feasibility studies Interpolation Mathematical models Nonlinear dynamics Proper Orthogonal Decomposition Radiative heat transfer Reduced order models Scale models Spacecraft Spacecraft environments Spacecraft models Subspace methods Temperature effects Thermal analysis Thermodynamic properties
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