Design of fuzzy logic guidance law against high-speed target
CL Lin, YY Chen - Journal of Guidance, Control, and Dynamics, 2000 - arc.aiaa.org
CL Lin, YY Chen
Journal of Guidance, Control, and Dynamics, 2000•arc.aiaa.orgQ= dynamic pressure Stref= reference area of ballistic target s= referencearea T= thrust v=
missile speed vt= target speed W= target weight x= horizontal coordinate a= angle of attack
b= ballistic coeffi cient c= ight-path angle ct= reentry angle of target d= velocity angle error
h= inertial line-of-sightangle l= induced drag coeffi cient q= atmospheric density r= heading
error angle
missile speed vt= target speed W= target weight x= horizontal coordinate a= angle of attack
b= ballistic coeffi cient c= ight-path angle ct= reentry angle of target d= velocity angle error
h= inertial line-of-sightangle l= induced drag coeffi cient q= atmospheric density r= heading
error angle
Q= dynamic pressure Stref= reference area of ballistic target s= referencearea T= thrust v= missile speed vt= target speed W= target weight x= horizontal coordinate a= angle of attack b= ballistic coeffi cient c= ight-path angle c t= reentry angle of target d= velocity angle error h= inertial line-of-sightangle l= induced drag coeffi cient q= atmospheric density r= heading error angle
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