Adaptive Polynomial Guidance With Impact Angle Constraint Under Varying Velocity

Adaptive Polynomial Guidance With Impact Angle Constraint Under Varying Velocity

Considering the velocity of the missile cannot remain constant in most applications due to the effect of aerodynamic drag and thrust, a feasible adaptive impact angle control guidance law under varying velocity is proposed. The design of the guidance command is transformed into the design of the fli...

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Bibliographic Details
Main Authors: Zhongtao Cheng, Bo Wang, Lei Liu, Yongji Wang
Format: Article
Language:English
Published: IEEE 2019-01-01
Series:IEEE Access
Subjects:
Impact angle
adaptive scheme
varying velocity
polynomial guidance
Online Access:https://ieeexplore.ieee.org/document/8766976/

Internet

https://ieeexplore.ieee.org/document/8766976/

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