DocumentCode :
1345392
Title :
The proportional navigation dilemma-pure or true?
Author :
Shukla, U.S. ; Mahapatra, P.R.
Author_Institution :
Dept. of Aerosp. Eng., Indian Inst. of Sci., Bangalore, India
Volume :
26
Issue :
2
fYear :
1990
fDate :
3/1/1990 12:00:00 AM
Firstpage :
382
Lastpage :
392
Abstract :
Two generic classes of proportional navigation (PN) laws are compared in detail. One class consists of pursuer-velocity-referenced systems, which include pure proportional navigation (PPN) and its variants; the second category consists of line-of-sight- (LOS-) referenced systems such as true proportional navigation (TPN), generalized true proportional navigation (GTPN), and generalized guidance laws. The existing closed-form solutions are discussed in detail, and the classical linear and quasilinear analytical solutions are summarized. A critical comparison is then made with regard to the definition, implementation, and analytical aspects of the guidance laws, including the method, the nature of solution, and an appraisal of the behavior of the pursuer motion resulting from the laws. It is established that, in spite of some restricted advantages in the solvability of the equations of motion, the LOS-referenced PN schemes suffer from serious limitations in terms of implementation and trajectory behavior. Among the major drawbacks are forward velocity variation requirement, relatively large control effort requirement, restrictions on initial engagement conditions to ensure intercept, lack of robustness, and possibility of unbounded acceleration. It is concluded that PPN is a better guidance law in a practical sense than TPN and its generalizations
Keywords :
missiles; navigation; closed-form solutions; guidance laws; line of sight referenced system; linear solution; pure proportional navigation; pursuer motion; pursuer-velocity-referenced systems; quasilinear analytical solutions; robustness; tactical guided missiles; true proportional navigation; unbounded acceleration; Acceleration; Appraisal; Closed-form solution; Force control; Missiles; Motion analysis; Navigation; Optical control; Proportional control; Velocity control;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.53445
Filename :
53445
Link To Document :
بازگشت