scholarly journals Integrated Strapdown Missile Guidance and Control With Field-of-View Constraint and Actuator Saturation

IEEE Access ◽  
2020 ◽  
Vol 8 ◽  
pp. 123623-123638
Author(s):  
Jiayi Tian ◽  
Haifeng Chen ◽  
Xuancen Liu ◽  
Huabo Yang ◽  
Shifeng Zhang
Keyword(s):  
Actuator Saturation ◽  
Field Of View ◽  
Missile Guidance ◽  
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.

An unsteady simulation technique for missile guidance and control applications

1997 ◽  
Author(s):  
L. Hall ◽  
C. Mitchell ◽  
V. Parthasarathy ◽  
L. Hall ◽  
C. Mitchell ◽  
...  
Keyword(s):  
Simulation Technique ◽  
Missile Guidance ◽  
Control Applications ◽  
Guidance And Control ◽  
Unsteady Simulation ◽  
And Control

Adaptive integrated guidance and control for impact angle constrained interception with actuator saturation

2019 ◽  
Vol 123 (1267) ◽  
pp. 1437-1453
Author(s):  
X. L. Ai ◽  
Y. C. Shen ◽  
L. L. Wang
Keyword(s):  
Actuator Saturation ◽  
Fixed Time ◽  
Impact Angle ◽  
Guidance And Control ◽  
Inherent Problem ◽  
Saturation Constraint ◽  
Integrated Guidance And Control ◽  
The Stability ◽  
And Control ◽  
Derivatives Of

ABSTRACTThis paper considers the integrated guidance and control (IGC) problem for impact angle constrained interception against manoeuvring targets with actuator saturation constraint. Based on the backstepping technique, an adaptive IGC law is presented to address this problem, where a fixed-time differentiator is proposed to estimate the derivatives of virtual control inputs to avoid the inherent problem of “explosion of complexity” suffered by the typical backstepping. Furthermore, an auxiliary first-order filter is introduced into the IGC law to cope with the actuator saturation constraint. The stability of the closed-loop system is strictly proved. Finally, the superiority of the proposed IGC law is verified by comparison simulations.

Integrated guidance and control for missile with narrow field-of-view strapdown seeker

2020 ◽  
Vol 106 ◽  
pp. 124-137
Author(s):  
Jiayi Tian ◽  
Neng Xiong ◽  
Shifeng Zhang ◽  
Huabo Yang ◽  
Zhenyu Jiang
Keyword(s):  
Field Of View ◽  
Guidance And Control ◽  
Integrated Guidance And Control ◽  
And Control

Partial integrated missile guidance and control with state observer

2014 ◽  
Vol 79 (4) ◽  
pp. 2497-2514 ◽  
Author(s):  
Xianghua Wang ◽  
Jinzhi Wang ◽  
Gang Gao
Keyword(s):  
State Observer ◽  
Missile Guidance ◽  
Guidance And Control ◽  
And Control
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