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Control of static unstable airframes 被引量:2
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作者 Junfang Fan defu lin +1 位作者 Zhong Su Qing Li 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2010年第6期1063-1071,共9页
The challenge and control problems of static unstable missiles are presented. The steady-state benefits of static instability are illustrated, while the corresponding control challenge is described both by the charact... The challenge and control problems of static unstable missiles are presented. The steady-state benefits of static instability are illustrated, while the corresponding control challenge is described both by the characteristic lag of airframe and the increment of necessary control usage. Control limitation led by unstable zero-pole pair is analyzed for preliminary design and evaluation. Linear control strategy is examined wherein two and three loop acceleration autopilots with different control usages are developed using an optimal control approach combined with frequency domain constraint. The weights selection and relation with system performance are detailed. Then the nonlinear backstepping recursive method is detailed to determine how well it is able to follow command and its engineering feasibility. The results show that a static unstable missile is controllable, while the actuator bandwidth is the crucial limited factor. There should be a compromise between overall performance and actuator payment. 展开更多
关键词 missile control static instability optimal control BACKSTEPPING weight matrix unstable zero-pole pair.
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UnIC: Towards Unmanned Intelligent Cluster and Its Integration into Society
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作者 Fubiao Zhang Jing Yu +1 位作者 defu lin Jun Zhang 《Engineering》 SCIE EI CAS 2022年第5期24-38,共15页
Collaborative unmanned systems have emerged to meet our society’s wide-ranging grand challenges,with their advantages including high performance,efficiency,flexibility,and inherent resilience.Increasing levels of gro... Collaborative unmanned systems have emerged to meet our society’s wide-ranging grand challenges,with their advantages including high performance,efficiency,flexibility,and inherent resilience.Increasing levels of group/team autonomy have also been achieved due to the embodiment of artificial intelligence(AI).However,the current networked unmanned systems are primarily designed for and applicable to a narrow range of domain-specific missions,and do not have sufficient human-level intel-ligence and human needs fulfillment for the challenging missions in our lives.We propose in this paper a vision of human-centric networked unmanned systems:Unmanned Intelligent Cluster(UnIC).Within this vision,distributed unmanned systems and humans are connected via knowledge sharing and social awareness to achieve collaborative cognition.This paper details UnIC’s concept,sources of intelligence,and layered architecture,and reviews enabling technologies for achieving this vision.In addition to the technological aspects,the social acceptance issues are highlighted. 展开更多
关键词 Unmanned intelligent systems Human centric systems Social intelligence Social acceptance Socio-technical systems
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Editorial for the Special Issue on Unmanned Intelligent Cluster
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作者 Jun Zhang Toshio Fukuda +1 位作者 defu lin Florian Holzapfel 《Engineering》 SCIE EI CAS 2022年第5期1-2,共2页
Recent advances in networked cooperative autonomous sys-tems offer the potential to significantly improve system quality for a wide range of applications.Progress in embedded processor,sensor,communication,and network... Recent advances in networked cooperative autonomous sys-tems offer the potential to significantly improve system quality for a wide range of applications.Progress in embedded processor,sensor,communication,and networking technology in the last few decades has accelerated interest in networked cooperative autonomous systems,multirobot systems,and distributed sensor networks for applications such as manufacturing,logistics,pro-cess monitoring,enhanced situational awareness,plant safety,inspection,security,and rescue operations. 展开更多
关键词 ROBOT NETWORKS AUTONOMOUS
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Impact time control guidance against maneuvering targets based on a nonlinear virtual relative model
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作者 Yuru BIN Hui WANG +2 位作者 defu lin Yaning WANG Xin SUN 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2023年第7期444-459,共16页
Aiming at the problem of high-precision interception of air-maneuvering targets with impact time constraints,this paper proposes a novel guidance law based on a nonlinear virtual relative model in which the origin is ... Aiming at the problem of high-precision interception of air-maneuvering targets with impact time constraints,this paper proposes a novel guidance law based on a nonlinear virtual relative model in which the origin is attached to the target.In this way,the original maneuvering target is transformed into a stationary one.A polynomial function of the guidance command in the range domain with two unknown coefficients is introduced into the virtual model,one of the coefficients is determined to achieve the impact time constraint,and the other is determined to satisfy a newly defined virtual look angle constraint.For meeting the terminal constraints simultaneously,the guidance command can finally be obtained.The resulting solution is represented as a combination of proportional navigation guidance-like term which is aimed to meet the zero miss distance constraint,a bias term for impact time control by adjusting the length of the homing trajectory,and an additional term for target maneuvers.Numerous simulations demonstrate that the proposed law achieves an acceptable impact time error for various initial conditions against different types of maneuvering targets and shows more effective performance in comparison with those of other existing guidance laws. 展开更多
关键词 Impact time control Maneuvering targets Polynomial guidance Virtual relative model Virtual look angle constraint
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