Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems

Author:	Curfman, Howard J.
Year:	1955
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L54L06a
Series:	NACA research memorandum ;
Report Number:	L54L06a
Subjects:	Guided missiles--Control systems--Aerodynamics
	Guidance systems (Flight)--Aerodynamics
Link:	https://hdl.handle.net/2027/mdp.39015086490433