A New Optimal Guidance Law for Homing Missiles with Varying Velocity
International sessions; 14th, Japan Society for Aeronautical and Space Sciences; Proceedings of JSASS 14th international sessions in 38th aircraft symposium ; 2000 ; Sendai, Japan
01.01.2000
4 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
On Optimal Guidance for Homing Missiles
AIAA | 1979
|Neoclassical Guidance for Homing Missiles
AIAA | 2001
|Generalized guidance law for homing missiles
Tema Archiv | 1989
|Maximum-information guidance for homing missiles
AIAA | 1984
|Maximum-information guidance for homing missiles
AIAA | 1985
|