A third-order solution of Vinti's problem with explicit expressions for the poisson brackets

1981 ◽  
Vol 5 (2) ◽  
pp. 192-201 ◽  
Author(s):  
Wu Lian-da ◽  
Tong Fu
2007 ◽  
pp. 53-60 ◽  
Author(s):  
R. Pavlovic

To apply the theorem of Nekhoroshev (1977) to asteroids, one first has to check whether a necessary geometrical condition is fulfilled: either convexity, or quasi-convexity, or only a 3-jet non-degeneracy. This requires computation of the derivatives of the integrable part of the corresponding Hamiltonian up to the third order over actions and a thorough analysis of their properties. In this paper we describe in detail the procedure of derivation and we give explicit expressions for the obtained derivatives. .


1986 ◽  
Vol 114 ◽  
pp. 127-127 ◽  
Author(s):  
W. Thuillot ◽  
D. T. Vu ◽  
J. E. Arlot

The two manners to improve the knowledge of the motions of the galilean satellites are the elaboration of a new theory and the use of high precision observations. In this paper, we present new results on these subjects.We have applied the Sagnier's method in order to get a new theory of the motions and we describe here the second approximation which leads to a third order solution. In this solution appear coupled terms in longitude of the perijoves and longitudes of the nodes. The de Haerdtl's inequalities, which come from the 3-7 commensurability between satellites 3 and 4 are included in this solution. These developments, first computed by de Heardtl, have been improved by Lieske (1973). In our solution we introduce the use of the variables in inclination, and some new terms appear.In order to get the best precision for the final ephemerides, the accuracy of the observations have to be improved: best results may be obtained with the use of the observations of mutual events. Simulations have shown the interest to take into account the variations of the albedo as a function of geographic longitudes and latitudes on the satellites themselves. So, the theoretical flux of light is closer to the observed one and the accuracy is improved. In 1985, mutual events occur and we have organized a campaign in order to obtain results of high precision.


1978 ◽  
Vol 41 ◽  
pp. 241-257
Author(s):  
Hiroshi Kinoshita

AbstractA third-order solution is developed for the motions of artificial satellites moving in the gravitational field of the Earth, whose potential includes the second-, third-, and fourth-order zonal harmonics. Third-order periodic perturbations with fourth-order secular perturbations are derived by Hori’s perturbations method. All quantities are expanded into power series of the eccentricity, but the solution is obtained so as to be closed with respect to the inclination. A comparison with the results of numerical integration of the equations of motion indicates that the solution can predict the position of a close-earth satellite with a small eccentricity with an accuracy of better than 1 cm over 1 month.


1988 ◽  
Vol 37 (3-4) ◽  
pp. 193-200 ◽  
Author(s):  
D. Ray ◽  
U. S. Jadhav

Kumar(l986) has proposed the criterion of third order moment for the identification of bilinear time series model and discussed its properties with respect to a simple bilinear model, In this paper, we have derived the explicit expressions of third order moment with respect to two terms diagonal model and discussed their properties in identifying the structure of a diagonal model.


2021 ◽  
Vol 33 (9) ◽  
pp. 097101
Author(s):  
Zhe Gao ◽  
Z. C. Sun ◽  
S. X. Liang

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