An implementable high-order guidance law for homing missiles

2002 ◽  
Author(s):  
R. Aggarwal ◽  
D. Boudreau
Keyword(s):  
High Order ◽  
Guidance Law ◽  
Homing Missiles

A new guidance law for homing missiles

1985 ◽  
Vol 8 (3) ◽  
pp. 402-404 ◽  
Author(s):  
Y. S. Kim ◽  
H. S. Cho ◽  
Z. Bien
Keyword(s):  
Guidance Law ◽  
Homing Missiles

An observer-based continuous adaptive sliding mode guidance against chattering for homing missiles

2019 ◽  
Vol 41 (12) ◽  
pp. 3309-3320 ◽  
Author(s):  
Jianguo Guo ◽  
Yifei Li ◽  
Jun Zhou
Keyword(s):  
Sliding Mode ◽  
Dimensional Space ◽  
Lyapunov Theory ◽  
Closed Loop System ◽  
Adaptive Function ◽  
Adaptive Sliding Mode ◽  
Guidance Law ◽  
Nonlinear Extended State Observer ◽  
The Stability ◽  
Homing Missiles

A novel observer-based continuous adaptive sliding mode guidance (OCASMG) is proposed for homing missiles. First, a new sliding mode guidance law is derived from the nonlinear dynamics describing the pursuit situation of a missile and a target in the two-dimensional space, where a continuous adaptive function is introduced to overcome the chattering problem in sliding mode. Second, to improve the accuracy of target interception, a new nonlinear extended state observer (NESO) is presented to estimate target acceleration and compensate for the sliding mode guidance law. The stability of observer-based closed-loop system is proved by Lyapunov theory. Finally, simulations are conducted on the nonlinear longitudinal missile model and results demonstrate the effectiveness of proposed method.

scholarly journals A Novel Penetration-evade Guidance Law against Two Homing Missiles

2018 ◽  
Vol 408 ◽  
pp. 012030
Author(s):  
Siyu Xiong ◽  
Gang Li ◽  
Siyu Huang ◽  
Jia Zhan
Keyword(s):  
Guidance Law ◽  
Homing Missiles
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