Closed-Form Solution of Pure Proportional Navigation

IEEE Transactions on Aerospace and Electronic Systems

Volumn 26, Issue 3, 1990, Pages 526-533

  Becker, Klaus ^a  

^a Forschungsinstitut fuer Funk und Mathematik Abteilung SuS ^*  (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EQUATIONS OF MOTION; NAVIGATION;

MISSILE-TARGET LINE OF SIGHT (LOS); PROPORTIONAL NAVIGATION (PN); UNBOUNDED MISSILE ACCELERATION;

ROCKETS AND MISSILES;

EID: 0025427757     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.106131     Document Type: Article

References (8)

1. Locke, A.S. (1960) Guidance. Princeton, NJ: Van Nostrand, 1955.
2. Guelman, M. (1971) A qualitative study of proportional navigation. IEEE Transactions on Aerospace and Electronic Systems, AES-7 (July 1971), 637–643.
3. Murtaugh, S.A., and Criel, H.E. (1966) Fundamentals of proportional navigation. IEEE Spectrum, 3 (Dec. 1966), 75–85.
4. Guelman, M. (1976) The closed-form solution of true proportional navigation. IEEE Transactions on Aerospace and Electronic Systems, AES-12 (July 1976), 472–482.
5. Yang, C.D., Yeh, F.B., and Chen, J.H. (1987) The closed-form solution of generalized proportional navigation. Journal of Guidance, Control and Dynamics, 10 (Mar.-Apr. 1987), 216–218.
6. Jerger, J.J. (1960) Systems Preliminary Design. Princeton, NJ: Van Nostrand, 1960.
7. Shukla, U.S., and Mahapatra, P.R. (1988) Generalized linear solution of proportional navigation. IEEE Transactions on Aerospace and Electronic Systems, AES-24 (May 1988), 231–238.
8. Gradshteyn, I.S., and Ryzhik, I.M. (1965) Table of Integrals, Series and Products. New York: Academic Press, 1965.