The closed-form solution of the equations of motion of an ideal missile pursuing a nonmaneuvering target according to the true propotional 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
IEEE Transactions on Aerospace and Electronic Systems ; AES-12 , 4 ; 472-482
01.07.1976
2261462 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
The closed-form solution of true proportional navigation
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