Titlebook: Optimal Guidance and Its Applications in Missiles and UAVs; Shaoming He,Chang-Hun Lee,Antonios Tsourdos Book 2020 The Editor(s) (if applic

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Shaoming He,Chang-Hun Lee,Hyo-Sang Shin,Antonios Tsourdoschoice of geometric and symbolic transformations that are necessary to achieve a particular visualization. Designers of map-like visualizations are thus challenged to seriously consider the implications of particular computational techniques and the consequences of symbolization choices.

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Book 2020e laws. In practice, this information is important in ensuring confidence in the performance and reliability of the guidance law when implementing it in a real-world system, especially in aerospace engineering where reliability is the first priority..

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Optimal Guidance and Its Applications in Missiles and UAVs

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Optimal Error Dynamics in Missile Guidanceptimal error dynamics for guidance law design to achieve various operational objectives. The proposed optimal error dynamics is derived by solving a linear quadratic optimal control problem through Schwarz’s inequality approach. The properties of the proposed optimal error dynamics are discussed. Th

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Optimal Trajectory Shaping Guidance Law with Seeker’s Field-of-View ConstraintThe proposed guidance law is derived by using the concept of biased PNG (BPNG). The guidance law developed leverages a nonlinear function to ensure the boundedness of velocity lead angle to cater for seeker’s FOV constraint. The finite-time convergence of the impact time error and impact angle error

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