Integrated guidance and control of advanced interceptors using second order sliding modes

2004 ◽  
Author(s):  
Y.B. Shtessel ◽  
I.A. Shkolnikov
Keyword(s):  
Second Order ◽  
Sliding Modes ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
And Control

Lateral guidance and control of UAVs using second-order sliding modes

2016 ◽  
Vol 49 ◽  
pp. 88-100 ◽  
Author(s):  
Syed Ussama Ali ◽  
Raza Samar ◽  
M. Zamurad Shah ◽  
Aamer I. Bhatti ◽  
Khalid Munawar ◽  
...  
Keyword(s):  
Second Order ◽  
Sliding Modes ◽  
Guidance And Control ◽  
And Control

scholarly journals MISSILE INTERCEPTOR GUIDANCE AND CONTROL USING SECOND ORDER SLIDING MODES

2005 ◽  
Vol 38 (1) ◽  
pp. 854-859 ◽  
Author(s):  
Yuri B. Shtessel ◽  
Ilya A. Shkolnikov ◽  
Arie Levant
Keyword(s):  
Second Order ◽  
Sliding Modes ◽  
Guidance And Control ◽  
And Control

Integral barrier Lyapunov functions-based integrated guidance and control design for strap-down missile with field-of-view constraint

2021 ◽  
pp. 014233122098132
Author(s):  
Bin Zhao ◽  
Zhenxin Feng ◽  
Jianguo Guo
Keyword(s):  
Sliding Mode ◽  
State Equation ◽  
Field Of View ◽  
Feedback Form ◽  
Theoretical Derivation ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
Twisting Algorithm ◽  
And Control ◽  
Special Time

The problem of the integrated guidance and control (IGC) design for strap-down missile with the field-of-view (FOV) constraint is solved by using the integral barrier Lyapunov function (iBLF) and the sliding mode control theory. Firstly, the nonlinear and uncertainty state equation with non-strict feedback form for IGC design is derived by using the strap-down decoupling strategy. Secondly, a novel adaptive finite time disturbance observer is proposed to estimate the uncertainties based on an improved adaptive gain super twisting algorithm. Thirdly, the special time-varying sliding variable is designed and the iBLF is employed to handle the problem of FOV constraint. Theoretical derivation and simulation show that the IGC system is globally uniformly ultimately bounded and the FOV angle constraint is also guaranteed not only during the reaching phase but also during the sliding mode phase.

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