Control decoupling analysis for gyroscopic effects in rolling missiles
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[1] D. Stallard. Decoupling the flight control system of a cruciform missile , 1976 .
[2] Peter N. Nikiforuk,et al. FREQUENCY RESPONSE ANALYSIS OF TWO-DIMENSIONAL NONLINEAR SYMMETRICAL AND NON-SYMMETRICAL CONTROL SYSTEMS, , 1968 .
[3] D. Newman,et al. The analysis of cross-coupling effects on the stability of two-dimensional, orthogonal, feedback control systems , 1960 .
[4] B. O. Lange,et al. Control synthesis for spinning aerospace vehicles. , 1967 .
[5] C. Murphy. Symmetric Missile Dynamic Instabilities , 1981 .
[6] Charles H. Murphy. Subharmonic Behavior of a Slightly Asymmetric Missile , 1973 .
[7] Joseph Shinar,et al. Dynamic analysis of beam-rider missile performance , 1979 .
[8] J. Shinar,et al. Effect of periodic roll rate in missiles with proportional navigation , 1976 .
[9] P. W. Fortescue,et al. The Generalized Root Locus (G.R.L.) method (for similar systems with antisymmetric coupling) , 1976 .
[10] James D. Iversen. Correlation of Magnus Force Data for Slender Spinning Cylinders , 1973 .
[11] W. J. G. Pinsker. The Theory and Practice of Inertia Cross-Coupling , 1969, The Aeronautical Journal (1968).