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Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2020.106334
Abstract: Abstract The skid-to-turn hypersonic vehicle is subject to the complex aerodynamic uncertainty and random wind disturbance. Besides, actuator saturation and full state constraints, consisting of attack angle, sideslip angle, bank angle and body angular rates…
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Keywords:
guidance control;
finite time;
multi constraints;
constraints adaptive ... See more keywords
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Published in 2019 at "International Journal of Systems Science"
DOI: 10.1080/00207721.2019.1587544
Abstract: ABSTRACT An integrated guidance and control scheme is proposed on path following for the unmanned aerial vehicle. It is capable of handling the coupled non-linearities of the path's kinematics and the aircraft's dynamics independently. In…
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Keywords:
guidance control;
control;
integrated guidance;
guidance ... See more keywords
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Published in 2017 at "Aircraft Engineering and Aerospace Technology"
DOI: 10.1108/aeat-12-2014-0209
Abstract: Purpose The purpose of this paper is to design an adaptive nonlinear controller for a nonlinear system of integrated guidance and control. Design/methodology/approach A nonlinear integrated guidance and control approach is applied to a homing,…
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Keywords:
integrated guidance;
guidance control;
control;
adaptive backstepping ... See more keywords
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Published in 2023 at "IEEE Transactions on Aerospace and Electronic Systems"
DOI: 10.1109/taes.2022.3199196
Abstract: Coverage path planning with unmanned aerial vehicles (UAVs) is a core task for many services and applications including search and rescue, precision agriculture, infrastructure inspection and surveillance. This work proposes an integrated guidance and gimbal…
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Keywords:
integrated guidance;
coverage;
control;
guidance gimbal ... See more keywords
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Published in 2020 at "Transactions of the Institute of Measurement and Control"
DOI: 10.1177/0142331219897430
Abstract: An integrated guidance and control (IGC) is designed in this study for a surface-to-air missile considering burned or broken fin as a fault. The IGC model in the pitch plane is developed with various uncertainties…
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Keywords:
guidance control;
sliding mode;
control;
fin ... See more keywords
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Published in 2022 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
DOI: 10.1177/09544100221103320
Abstract: In this study, a novel three-dimensional continuous-time integrated guidance and control (IGC) scheme is presented. The proposed method is developed on the basis of generalized model predictive control (GMPC) approach and super-twisting extended state observer…
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Keywords:
dimensional continuous;
continuous time;
integrated guidance;
time integrated ... See more keywords
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Published in 2019 at "Journal of Aerospace Technology and Management"
DOI: 10.5028/jatm.v11.982
Abstract: Based on adaptive sliding mode-control and back-stepping design method, an integrated guidance and control method with less calculation is proposed, which is designed for air-to-ground missile during the terminal course in threedimensional space. The model…
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Keywords:
sliding mode;
control;
integrated guidance;
guidance control ... See more keywords