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Issue on page /notebooks/06.04-Soft-Landing-Apollo-11-on-the-Moon.html #44
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Actually, (answering my own question), something along the lines of :
for the initial conditions produces a solution. |
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First , let me say thank you for your work with Pyomo, amazing software!
In the Soft landing example : 6.4.3. Version 2: Rescaled model, the boundary conditions are provided for the altitude (h_initial = 100000.0 m) and the orbital velocity (v_initial = 1520 m/s)
I noticed that for the normalized formulation above, v(tau)=v(t)*T (T=final time) so the initial velocity provided is not scaled appropriately. That result in a velocity profile:
vsim = np.array([m.v[t]()/m.T() for t in m.t])
that does not match the 1520 m/s boundary conditions at t=0.
I suggest updating the example. (Also, is there an obvious work-around to specify boundary condition for the derivatives in a normalized setting?).
Best,
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