Nonlinear analysis of a simple model of temperature evolution in a satellite

[1]  P. G. Drazin,et al.  Nonlinear systems: Frontmatter , 1992 .

[2]  V. Arnold,et al.  Ordinary Differential Equations , 1973 .

[3]  M. Hirsch,et al.  Differential Equations, Dynamical Systems, and Linear Algebra , 1974 .

[4]  Vimal Singh,et al.  Perturbation methods , 1991 .

[5]  Jih-Run Tsai,et al.  Overview of satellite thermal analytical model , 2004 .

[6]  Stanley Burris,et al.  Counting Rooted Trees: The Universal Law t(n)~C ρ-n n-3/2 , 2006, Electron. J. Comb..

[7]  J. Bell,et al.  Counting Rooted Trees: The Universal Law $t(n)\,\sim\,C \rho^{-n} n^{-3/2}$ , 2006 .

[8]  Isabel Pérez-Grande,et al.  Transient thermal analysis during the ascent phase of a balloon-borne payload. Comparison with SUNRISE test flight measurements , 2009 .

[9]  Linearized techniques for solving the inverse problem in the satellite thermal control 1 1 Paper IAF , 1998 .

[10]  N. G. Parke,et al.  Ordinary Differential Equations. , 1958 .

[11]  R. Otter The Number of Trees , 1948 .

[12]  S. Orszag,et al.  Advanced Mathematical Methods For Scientists And Engineers , 1979 .

[13]  S. E. Khaikin,et al.  Theory of Oscillators , 1966 .

[14]  I. Pérez-Grande,et al.  Analytical study of the thermal behaviour and stability of a small satellite , 2009 .

[15]  鈴木 増雄 A. H. Nayfeh and D. T. Mook: Nonlinear Oscillations, John Wiley, New York and Chichester, 1979, xiv+704ページ, 23.5×16.5cm, 10,150円. , 1980 .

[16]  Y. Oshima,et al.  An Analytical Approach to the Thermal Design of Spacecrafts , 1968 .

[17]  M. Gadalla Prediction of temperature variation in a rotating spacecraft in space environment , 2005 .