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Published in 2018 at "International Journal of Automation and Computing"
DOI: 10.1007/s11633-016-0953-y
Abstract: In order to improve the precision of guidance for the missile intercepting maneuvering targets, this paper proposes a sliding mode guidance law with impact angle constraints based on the equation of the relative motion of…
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Keywords:
impact angle;
sliding mode;
guidance law;
guidance ... See more keywords
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Published in 2018 at "International Journal of Aeronautical and Space Sciences"
DOI: 10.1007/s42405-018-0004-8
Abstract: This paper proposes a guidance law which considers the constraints of seeker field-of-view (FOV) as well as the requirements on impact angle and time. The proposed guidance law is designed for a constant speed missile…
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Keywords:
impact angle;
field view;
guidance law;
angle time ... See more keywords
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Published in 2021 at "Applied Ocean Research"
DOI: 10.1016/j.apor.2020.102488
Abstract: Abstract An improved adaptive integral line-of-sight guidance law and path following control system for Unmanned Surface Vehicles (USVs) with uncertainties is proposed in this paper. The dynamic equations of the tracking errors are established in…
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Keywords:
improved adaptive;
integral line;
adaptive integral;
guidance law ... See more keywords
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Published in 2020 at "Advances in Space Research"
DOI: 10.1016/j.asr.2019.10.008
Abstract: Abstract This paper researches the ascent guidance law for the vehicle with a multi-combined cycle propulsion. The guidance law comprises two parts, namely, the off-line optimal trajectories generation and online guidance. With respect to the…
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Keywords:
guidance law;
ascent guidance;
vehicle multi;
guidance ... See more keywords
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Published in 2018 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2018.05.018
Abstract: Abstract In this paper, a new optimal guidance law with terminal constraints on miss distance and intercept angle is proposed for a missile with time-varying velocity against a maneuvering target. The proposed optimal guidance law…
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Keywords:
tangent function;
intercept angle;
hyperbolic tangent;
guidance law ... See more keywords
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Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.105672
Abstract: Abstract In this paper, a new guidance law is proposed based on computational geometry with impact time and angle constraints against a stationary target in three dimensions. The law is based on the principle of…
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Keywords:
guidance law;
impact time;
geometry;
computational geometry ... See more keywords
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Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2019.105678
Abstract: Abstract This paper proposes a novel glide guidance law for the reusable launch vehicle (RLV), in which longitudinal and lateral paths are separately designed to quickly derive guidance commands. First, an altitude profile is designed…
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Keywords:
virtual target;
reusable launch;
guidance law;
glide guidance ... See more keywords
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Published in 2020 at "Aerospace Science and Technology"
DOI: 10.1016/j.ast.2020.105787
Abstract: Abstract In this paper, we propose a novel nonlinear cooperative interception guidance law for the target and the defender in a target-defender-chaser scenario. In particular, the cooperative guidance problem is converted to a two-input-two-output control…
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Keywords:
guidance law;
guidance;
interception guidance;
cooperative interception ... See more keywords
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Published in 2020 at "Chinese Journal of Aeronautics"
DOI: 10.1016/j.cja.2019.07.013
Abstract: Abstract Guidance laws are proposed for a near space interceptor with on–off type thrust as output. The target-interceptor engagement kinematics is integrated with the first-order dynamics of thruster to design guidance laws. The bang-bang type…
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Keywords:
finite time;
composite guidance;
guidance;
guidance law ... See more keywords
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Published in 2021 at "Chinese Journal of Aeronautics"
DOI: 10.1016/j.cja.2021.05.021
Abstract: Abstract The design of optimal guidance law for intercepting a near-space hypersonic maneuvering target with bounded inputs is considered. Firstly, a maneuvering model for near-space hypersonic aircraft is given. Then, the aircraft acceleration prediction can…
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Keywords:
near space;
sliding mode;
space hypersonic;
guidance law ... See more keywords
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Published in 2017 at "IFAC-PapersOnLine"
DOI: 10.1016/j.ifacol.2017.08.2351
Abstract: Abstract This article presents a new command shaping guidance law by change of Lagrange multiplier (LM), called CSGL-LM. The Schwarz inequality approach is used to solve the optimal guidance problems considering both terminal constraints on…
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Keywords:
command;
guidance law;
new command;
guidance ... See more keywords