Computation of the Different Errors in the Ballistic Missiles Range

Figure 1

(a) Geometry of a typical ICBM trajectory. (b) Some orbital parameters at the burnout point. where Γ,Ψ,Ω, and Λ are the powered flight, free flight, reentry, and total range angles, respectively, and 𝑅_𝑏,𝑅_𝑓𝑓,𝑅_𝑟𝑒,and𝑅_𝑡 are their ground ranges.

(a)

(b)