From d267c17827cc101213677c711f6218acce9dc427 Mon Sep 17 00:00:00 2001 From: Sofia Covarrubias <44685425+sofiacovarrubias@users.noreply.github.com> Date: Thu, 29 Feb 2024 11:40:00 -0800 Subject: [PATCH] formatting test --- docs/manual.rst | 49 ++++++++++++++++++++----------------------------- 1 file changed, 20 insertions(+), 29 deletions(-) diff --git a/docs/manual.rst b/docs/manual.rst index 6d82ab48..3e53d60e 100644 --- a/docs/manual.rst +++ b/docs/manual.rst @@ -25,7 +25,7 @@ of orbital parameters .. math:: \Delta R.A. = \pi a(1-ecosE)[cos^2{i\over 2}sin(f+\omega_p+\Omega)-sin^2{i\over 2}sin(f+\omega_p-\Omega)] - + \ \Delta decl. = \pi a(1-ecosE)[cos^2{i\over 2}cos(f+\omega_p+\Omega)+sin^2{i\over 2}cos(f+\omega_p-\Omega)] where 𝑎, 𝑒, :math:`\omega_p`, Ω, and 𝑖 are orbital parameters, and 𝜋 is the system parallax. f is @@ -34,14 +34,11 @@ through Kepler’s equation and Kepler’s third law .. math:: M = 2\pi ({t\over P}-(\tau -\tau_{ref})) - - + \ ({P\over yr})^2 =({a\over au})^3({M_\odot \over M_{tot}}) - - + \ M =E-esinE - - + \ f = 2tan^{-1}[\sqrt{{1+e\over 1-e}}tan{E\over 2}] ``orbitize!`` employs two Kepler solvers to convert between mean @@ -52,29 +49,23 @@ orbit. See `Blunt et al. (2020)