The closed form solution of the equations of motion of an ideal missile pursuing a nonmanoevering target according to the true proportional navigation law is obtained. An analysis of the solution is performed, and the conditions necessary for the missile to reach the target are determined.
The closed-form solution of true proportional navigation
Die geschlossene Loesung der wahren proportionalen Navigation
IEEE Transactions on Aerospace and Electronic Systems ; AES-12 , 4 ; 472-482
1976
11 Seiten, 4 Quellen
Aufsatz (Zeitschrift)
Englisch
The closed-form solution of true proportional navigation
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