Second-order version of ballistic missile attitude-control system, with thrust gimbal deflection limiting, is examined; exact stability boundaries are found, and Lyapunov boundary is derived as function of system parameters, which is identical to exact boundary in critical regions of system phase plane; third-order version, which includes gimbal dynamics, deflection limiting, and deflection rate limiting, is analyzed; exact boundaries in portion of phase space are found, and extension of second-order results is considered.
Missile attitude stabilization by Lyapunov's second method
J Spacecraft Rockets
Journal of Spacecraft and Rockets ; 1 , n 6
1964
7 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Control design of fin roll stabilization in beam seas based on Lyapunov's direct method
Online Contents | 2012
|Lyapunov's Stability of Nonlinear Misaligned Journal Bearings
Online Contents | 1995
|