that affect a missile control system

R.O. Mindlin L.E. Goodman Beam vibrations with time-dependent boundary conditions journal of Applied Mechanics ASME Transactions Vol 72 pp 377-380 December 1950

R.L. Bisplinghoff H. Ashley R.L. Halfman Aeroelasticity Addison-Wesley Publishing Company Inc Cambridge Massachusetts 1955

J.E. Stocker A.B. Clymer Structural analysis and simulation Structural Mechanics and Materials Research Memorandum SMMR TM 22-62 Columbus division North American Aviation Inc November 9 1962

A.B. Clymer Operational analog simulation of the vibration of a beam and a rectangular multicellular structure SIMULATION vol 3 no 1 pp 18-31 July 1964

B.F. Pearce I.L. Ashkenas W.A. Johnson Development and implications of lateral approximate longitudinal transfer functions for flexible airframes IAS paper no 62-92 Institute of the Aerospace Sciences 1962

W.C. Hurty On the dynamic analysis of structural systems using component modes AIAA paper no 64-487 Institute of Aerospace Sciences 1964 Washington DC

C.L. Dolph On the Timoshenko theory of transverse beam vibrations Quarterly of Applied Mathematics Vol XII no 2 pp 175-187 July 1954

J. Zaborzksky W.J. Luedde M.J. Wendl New flight control techniques for a highly elastic booster ASD Technical Report 61-231 Aeronautical Systems Division Wright-Patterson AFB Ohio September 1961

G.M. Andrew J.M. Johnson Jr Automatic control of aeroelastic modes IAS paper no 62-86 Institute of Aerospace Sciences Los Angeles 1962

A.G. Fonda F.J. Trueh Flexible flight vehicle transfer function factors for use in autopilot preliminary design Technical Documentary Report no RTD-63-4218 Air Force Flight Dynamics Laboratory Wright-Patterson AFB Ohio April 1964

G.E. Tutt W.K. Waymeyer Model feedback applied to flexible booster control IRE Transactions on Automatic Control Vol AC-6 no 2 pp 135-142 May 1961