<jupyter_start><jupyter_text>Orbital Relative Sheet (draft)Technical description of what this is:Implement the [Clohessy–Wiltshire equations](https://en.wikipedia.org/w/index.php?title=Clohessy–Wiltshire_equations) via the `scipy.integrate.solve_ivp` utility. In other words, this does an time-domain ODE solve with SciPy for a neighborhood of co-orbiting points (rotating reference frame).<jupyter_code># constants
mu = 3.986e14 # m3/s2
n = 0.00113 # seconds
def f(t, v):
    u, udot = v[:2], v[2:]
    udd = [0 for i in range(3)]  # 2nd deriv
    x = u[0]
    y = u[1]
    z = u[2]
    udd[0] = 3*(n**2)*x + 2*n*udot[1]
    udd[1] = -2*n*udot[0]
    udd[2] = -(n**2)*z
    # what are values for udot???<jupyter_output><empty_output>
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