Skip to main content

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 0−θ v0

[20,80]°

[−10,10]°

[−2,2]°/s

[−2,2]°/s

[0,10]°