Case | S/N | a | r | i | ![]() |
e | ![]() |
Shift Q/F | Shift U/F |
[AU] | [![]() |
[![]() |
[![]() |
[![]() |
[
![]() |
[
![]() |
|||
0.03a | 1.5 | 60 | 120 | 0.2 | 200 | -2.0 | -0.7 | ||
1 (Fig. 9) | 5.0 | ||||||||
0.03a | ![]() |
![]() |
![]() |
![]() |
![]() |
![]() |
![]() |
||
0.03a | 1.5 | 75 | 90 | 0.0 | -c | 1.0 | -0.5 | ||
2 (Fig. 10) | 1.5 | ||||||||
0.03a | ![]() |
![]() |
![]() |
0.0b | -c | ![]() |
![]() |
Notes. (a) Fixed parameter.
(b) The uncertainty of e is 0.04.
(c) Undefined parameter; fixed to 90
in the fitting procedure for eccentric orbits. In each case the top row
refers to the true parameters employed to simulate the data, while the
bottom row gives the result obtained from the
-minimization. The 1
errors correspond to the standard deviation of each parameter as obtained from the Monte Carlo simulations.
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