This thesis is an application of parameter sensitivity analysis to aerodynamic parameters of a Bank-to-Turn missile. In the development a brief review of trajectory sensitivity theory is presented. A linear analysis is performed using an Uncoupled Pitch Channel Autopilot and a Coupled Roll-Yaw Channel Autopilot of the missile taken as model. Finally, a nonlinear analysis is given for the system. Comparisons between the linear and nonlinear cases are outlined. (Author)
Application of Sensitivity Analysis to Aerodynamic Parameters of a Bank to Turn Missile
1983
250 pages
Report
No indication
English
Missile Guidance & Control Systems , Guided missile models , Aerodynamic configurations , Parametric analysis , Sensitivity , Guided missiles , Guided missile trajectories , Linear regression analysis , Nonlinear analysis , Automatic pilots , Roll , Yaw , Pitch(Motion) , Charts , Computer programs , Theses , Bank to turn missiles
Missile aerodynamic sensitivity analysis
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