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Table 2 Parameter ranges

From: Geometric optimal control and applications to aerospace

v 0 θ v0 ψ v0 θ 0 ψ 0
fixed 0.8 Mach [−10,0]° fixed 0° [−10,10]° fixed 0°
θ f ψ f ω x0 ω y0 θ 0θ v0
[20,80]° [−10,10]° [−2,2]°/s [−2,2]°/s [0,10]°