Remarks on the inertia instability of a rolling missile
Author:
Magnus Tideman
Journal:
Quart. Appl. Math. 20 (1962), 1-11
MSC:
Primary 70.99
DOI:
https://doi.org/10.1090/qam/137336
MathSciNet review:
137336
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Abstract: Lyapunov’s second method is applied to the question of stability when dynamic cross coupling is considered. The main result is a condition on the maximal non-symmetry that gives stable performance for any constant or non-constant angular velocity in roll. Methods are outlined for the treatment of some related questions.
- Ray E. Bolz, Dynamic stability of a missile in rolling flight, J. Aeronaut. Sci. 19 (1952), 395–403. MR 48981
W. M. Phillips, Effects of steady rolling on longitudinal and directional stability, NACA TN 1627, June 1948
- Charles H. Murphy Jr., Criteria for the generalized dynamic stability of a rolling symmetric missle, J. Aero. Sci. 24 (1957), 773–774. MR 93104
R. E. Bolz, Dynamic stability of a missile in rolling flight, J. Aeronaut. Sci. 19, No. 6, 395–403 (June 1952)
W. M. Phillips, Effects of steady rolling on longitudinal and directional stability, NACA TN 1627, June 1948
S. H. Murphy, Criteria for the generalized dynamic stability of a rolling symmetric missile, J. Aeronaut, sci. 24, 773–774 (1957)
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Article copyright:
© Copyright 1962
American Mathematical Society