Stability Limits for the Velocity Orientation Autopilot of Rolling Missiles

Stability Limits for the Velocity Orientation Autopilot of Rolling Missiles

In this paper, we derive the sufficient and necessary stability conditions for rolling missiles with velocity orientation autopilot. For the mathematical derivation, linear time-invariant mathematical models are established. Structures of the velocity orientation autopilot for nonrolling and rolling...

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Bibliographic Details
Main Authors: Shaoyong Hu, Jiang Wang, Yuchen Wang, Song Tian
Format: Article
Language:English
Published: IEEE 2021-01-01
Series:IEEE Access
Subjects:
Rolling missile
coning motion
velocity orientation autopilot
dynamic stability
stability improving methods
Online Access:https://ieeexplore.ieee.org/document/9504563/

Internet

https://ieeexplore.ieee.org/document/9504563/

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