Results 11 to 20 of about 75,283 (193)
Adaptive Super-Twisting Algorithm-Based Nonsingular Terminal Sliding Mode Guidance Law
Journal of Control Science and Engineering, 2020 A nonsingular fast terminal sliding mode guidance law with an impact angle constraint is proposed to solve the problem of missile guidance accuracy and impact angle constraint for maneuvering targets.
Fang Yang, Kuanqiao Zhang, Lei Yu
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Prescribed Performance Guidance Law with Multiple Constraints
International Journal of Aerospace Engineering, 2022 In the terminal guidance phase of intercepting aerial target, a guidance law, satisfying impact angle constraint, acceleration constraint, and second-order dynamic characteristic of interceptor autopilot, is designed based on the prescribed performance ...
Xu Li, Jikun Ye, Chijun Zhou, Xiao Tang
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Collaborative Trajectory Planning Method for Hypersonic Glide Vehicle [PDF]
Hangkong bingqi, 2022 In order to meet the time and angle requirements of hypersonic glide vehicle’s cooperative reentry, a multi-constraint cooperative reentry trajectory planning algorithm is proposed considering the process constraints and transition point constraints ...
Wang Xinyu, Liang Xuezhi, Shi Rui, Zhang Dong
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Multi-Objective Robust H-infinity Control of Spacecraft Rendezvous [PDF]
, 2009 Based on the relative motion dynamic model illustrated by C-W equations, the problem of robust Hinfin control for a class of spacecraft rendezvous systems is investigated, which contains parametric uncertainties, external disturbances and input ...
Gao, Huijun, Shi, Peng, Yang, Xuebo
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International Journal of Aerospace Engineering, 2022 Considering that the terminal impact angle constraint can improve the interception performance of hypersonic target, a novel particle swarm optimization guidance (NPSOG) algorithm is proposed to satisfy the impact angle constraint.
Fan He, Weiyi Chen, Yang Bao
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Generalized Guidance Formulation for Impact Angle Interception with Physical Constraints
Aerospace, 2021 This paper proposes an optimal impact angle control guidance law for homing missiles with a narrow field-of-view of the seekers. As groundwork for designing a guidance law, we first present a general guidance structure that can achieve any terminal ...
Hyeong-Geun Kim, Jun-Yong Lee
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Impact-Angle and Terminal-Maneuvering-Acceleration Constrained Guidance against Maneuvering Target
Aerospace, 2021 A new, highly constrained guidance law is proposed against a maneuvering target while satisfying both impact angle and terminal acceleration constraints.
Wanqing Zhang, Wanchun Chen, Wenbin Yu
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Integrated Guidance and Control with Input Saturation and Impact Angle Constraint
Discrete Dynamics in Nature and Society, 2020 Aiming at the problem of impact angle constraint and input saturation, an integrated guidance and control (IGC) algorithm with impact angle constraint and input saturation is proposed.
Zhenhua Fu +3 more
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Rear wheel torque vectoring model predictive control with velocity regulation for electric vehicles [PDF]
, 2015 In this paper we propose a constrained optimal control architecture for combined velocity, yaw and sideslip regulation for stabilisation of the vehicle near the limit of lateral acceleration using the rear axle electric torque vectoring configuration of ...
Longo, Stefano +2 more
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Optimal Alignments for Designing Urban Transport Systems: Application to Seville [PDF]
, 2019 The achievement of some of the Sustainable Development Goals (SDGs) from the recent 2030 Agenda for Sustainable Development has drawn the attention of many countries towards urban transport networks. Mathematical modeling constitutes an analytical tool
Marseglia, Guido +3 more
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