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