HOMING MISSILE AUTOPILOT RESPONSE SENSITIVITY TO STABILITY DERIVATIVE VARIATIONS.

Proceedings of the IEEE Conference on Decision and Control

Volumn , Issue , 1984, Pages 1116-1121

  Nesline, P William ^a   Nesline, Mark L ^a  

^a RAYTHEON COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS - STABILITY; CONTROL SYSTEMS - ROBUSTNESS;

AERODYNAMIC STABILITY DERIVATIVE; HOMING MISSILE AUTOPILOT; INTERCEPTION; MANEUVERING TARGET; RESPONSE SENSITIVITY;

ROCKETS AND MISSILES;

AERODYNAMIC STABILITY DERIVATIVE; HOMING MISSILE AUTOPILOT; INTERCEPTION; MANEUVERING TARGET; RESPONSE SENSITIVITY;

EID: 0021641968     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/cdc.1984.272187     Document Type: Conference Paper

References (5)