Delete orbiter/orbits/body.py

orbiter/orbits/body.py

@@ -1,57 +0,0 @@
-from enum import Enum
-import numpy as np
-
-from ..units import *
-from .calc import format_sig_figs
-
-class Body:
-    """
-    Base class for any orbital body
-    """
-    def __init__(self, X: Position, V: Velocity, m: Mass, name: str = ""):
-        """
-        x (position) and v (velocity) 
-        """
-        self.X = X
-        self.V = V
-        self.A = Acceleration([0,0,0])
-        self.m = m
-        self.name = name
-
-    def save(self):
-        return (self.X, self.V, self.m)
-    
-    @classmethod
-    def load(cls, tup):
-        return cls(tup[0], tup[1], tup[2])
-
-    def step(self, step_size: float):
-        self.X += step_size*self.V
-        self.V += step_size*self.A
-        self.A = HighPrecisionVector([0,0,0])
-    
-    def __str__(self):
-        pos = 'm '.join([format_sig_figs(real_pos(x), 3) for x in self.X])
-        vel = 'm/s '.join([format_sig_figs(real_vel(v), 3) for v in self.V])
-        return str(f"{self.name}: X = {pos}, V = {vel}")
-    
-    def E(self):
-        return self.ke() + self.pe()
-
-    def pe(self):
-        return -self.m/self.dist_from_o()
-
-    def dist_from_o(self):
-        return sum([x**2 for x in self.X]).sqrt()
-
-
-    def ke(self):
-        return Decimal(0.5)*self.m*(self._speed()**2)
-
-    def _speed(self):
-        return sum([v**2 for v in self.V]).sqrt()
-
-    def speed(self):
-        return str(f"{format_sig_figs(real_vel(self._speed),5)}")
-    
-