Solve lqr in Matlab with bintel thrust

[todo]

bintel/experiments/episodic_KEEDMD/fast_drone_landing/tune_learning.py

Lines 32 to 37 in e79ecff

	K = array([0.8670, 0.9248]) #TODO: Solve lqr in Matlab with bintel thrust
	g = 9.81
	A_nom = array([[0., 1.], [0., 0.]]) # Nominal model of the true system around the origin
	B_nom = array([[0.], [1./(hover_thrust/g)]]) # Nominal model of the true system around the origin
	A_cl = A_nom - dot(B_nom, K)
	nominal_sys = LinearSystemDynamics(A=A_nom, B=B_nom)

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This issue was generated by todo based on a TODO comment in e79ecff. It's been assigned to @Cafolkes because they committed the code.