Impact angle constraint guidance law using fully-actuated system approach
Aerospace Science and Technology, 2023Shi-wei Chen +3 more
semanticscholar +1 more source
Missile Guidance Law Considering Constraints on Impact Angle and Terminal Angle of Attack
AIAA Guidance, Navigation, and Control Conference, 2015This paper proposes a guidance law considering constraints on impact angle and terminal angle of attack for a homing missile. In the proposed structure, the guidance law generates angle of attack command and the controller tracks the generated command.
Hyeonggeun Kim, H Jin Kim
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Segmented Optimal Guidance with Constraints on Terminal Angle of Attack and Impact Angle
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2012Guidance law with constraint on both terminal ight path angle and terminal angle of attack was considered.Linearized missile airframe and rst order missile dynamics were taken into account to add the angle of attack as a state of the guidance equation.
Qiang Xing, Wanchun Chen
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A ballistic optimization method with field-of-view angle constraint and impact angle constraint
2023 2nd Conference on Fully Actuated System Theory and Applications (CFASTA), 2023Yongjin Feng +6 more
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Fractional-order sliding mode control based guidance law with impact angle constraint
Nonlinear dynamics, 2021Y. Sheng, Zhuo Zhang, Lei Xia
semanticscholar +1 more source
Fast Convergent Nonsingular Terminal Sliding Mode Guidance Law with Impact Angle Constraint
Cybersecurity and Cyberforensics Conference, 2018In this paper, a nonsingular, essentially continuous and finite time fast convergent guidance law with impact angle constraint for some missiles attacking the targets with zero miss-distance and terminal impact angle constraint is presented by using ...
Kuanqiao Zhang, Suo-chang Yang
semanticscholar +1 more source
Influence of initial heading angle for the optimal guidance law with impact angle constraint
2016 IEEE International Conference on Information and Automation (ICIA), 2016Control of impact angle can considerably increase missile's lethality. However, large impact angle will lead to large lateral acceleration requirement during the flight. In order to avoid command saturation, one can choose initial heading angle to decrease the magnitude of the guidance command.
Xingyuan Xu, Zhizhong Liao
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Fixed time integrated guidance and control with impact angle constraint
2020 IEEE 16th International Conference on Control & Automation (ICCA), 2020This study proposes a fixed-time integrated guidance and control (IGC) scheme to hit maneuvering targets for missiles with impact angle constraint. By combining backstepping technique, an IGC law is designed to achieve the impact angle converge to the expected impact angle within fixed time.
Xinghe Zhou +3 more
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Observer-based integrated guidance and control under terminal impact angle constraint
ACM Cloud and Autonomic Computing Conference, 2018Integrated guidance and control (IGC) design is an active research field in guided weapon system due to ability of utilizing measured information from both guidance loop and control loop.
Jiawei Jing, Liangyu Zhao, Zhiqi Niu
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Differential Game Missile Guidance with Impact Angle and Time Constraints
IFAC Proceedings Volumes, 2011Abstract Modern anti-ship missiles are required for enhancement of the survivability against anti-air defense systems of warships. In this paper, the linear quadratic differential game missile guidance law to control impact angle and time is proposed, which enables to take advantages of vulnerability of warships.
Seonhyeok Kang, H. Jin Kim
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