Modeling and Vertical Launch Analysis of an Aero and Thrust Vector Controlled Surface to Air Missile

[1]  Jack N. Nielsen The present status and the future of missile aerodynamics , 1989 .

[2]  Andrew B. Wardlaw,et al.  Induced Side Forces on Bodies of Revolution at High Angle of Attack , 1975 .

[3]  Daniel J. Lesieutre,et al.  High angle of attack missile aerodynamics including rotational rates - Program M3HAX , 1996 .

[4]  L. H. Jorgensen Prediction of static aerodynamic characteristics for slender bodies alone and with lifting surfaces to very high angles of attack , 1976 .

[5]  Kevin A. Wise,et al.  Agile missile dynamics and control , 1996 .

[6]  J. E. Fidler,et al.  Asymmetric Vortex Effects on Missile Configurations , 1975 .

[7]  P. Giragosian Aerodynamic consideration in the design of a vertically launched advanced interdiction missile /VLAIM/ , 1982 .

[8]  Robert H. Nunn,et al.  Aerodynamic Characteristics of an Axisymmetric Body Undergoing a Uniform Pitching Motion , 1975 .

[9]  Max F. Platzer,et al.  Aerodynamic characteristics of a canard-controlled missile at high angles of attack , 1993 .

[10]  Mario Innocenti,et al.  A sliding mode missile pitch autopilot synthesis for high angle of attack maneuvering , 1998, IEEE Trans. Control. Syst. Technol..

[11]  R. Solis An analysis of the vertical launch phase of a missile concept , 1983 .

[12]  Patrick Reisenthel,et al.  Development of a nonlinear indicial model for maneuvering fighter aircraft , 1996 .

[13]  Peiqing Liu,et al.  Experimental Investigation of Aerodynamic Characteristics on Slender Bodies at High Angles of Attack , 2003 .

[14]  Andrew B. Facciano,et al.  Evolved SeaSparrow Missile Jet Vane Control System Prototype Hardware Development , 2002 .

[15]  Melissa A. McDaniel,et al.  High Angle of Attack Aerodynamic Predictions Using Missile Datcom , 2005 .

[16]  Sangho Kim,et al.  Asymmetric Vortices around a Body at High Angle of Attack Supersonic Flow , 2009 .