This paper researches optimal end guidance law about homing UAV. After building mathematic model, simulation results show that optimal end guidance law (OEGL) attacking fixed targets is superior to constant coefficient proportion guidance law (CCPGL).
Research of Optimal End Guidance Law about Homing UAV
Applied Mechanics and Materials ; 415 ; 30-33
2013-09-03
4 pages
Article (Journal)
Electronic Resource
English
On optimal guidance for homing missiles
TIBKAT | 1978
|On Optimal Guidance for Homing Missiles
AIAA | 1979
|Research of Integrated Design about Guidance and Control of Homing UAV
Trans Tech Publications | 2013
|NTIS | 1971
|An analysis of optimal command guidance vs. optimal semi-active homing missile guidance
Tema Archive | 1986
|