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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Optimal Guidance and Its Applications in Missiles and UAVs978-3-030-47348-8Series ISSN 1869-1730 Series E-ISSN 1869-1749

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Shaoming He,Chang-Hun Lee,Antonios TsourdosProvides a valuable resource for engineers working on optimal guidance and control systems, as well as graduate students majoring in aerospace engineering.Presents numerical simulations that clearly d

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https://doi.org/10.1007/978-3-030-47348-8Missile Guidance; Guidance Law; aerospace engineering; aerospace vehicles; unmanned aerial vehicles; traj

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形容词

Introduction of Optimal Guidance,re the characteristics of classical proportional navigation guidance and present the motivation of the development of new optimal guidance laws in this chapter. The overall aim of this book is then summarized and the organization of the entire book, together with some highlights of each chapter, are presented.

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Minimum-Effort Waypoint-Following Guidance Law laws developed can be applied to general waypoint-following missions with an arbitrary number of waypoints and an arbitrary number of arrival angle constraints. Nonlinear numerical simulations clearly demonstrate the effectiveness of the proposed formulations.

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Optimal Trajectory Shaping Guidance Law with Seeker’s Field-of-View Constraint is theoretically analyzed. By investigating the optimality of the biased command, the physical meaning of the proposed trajectory shaping guidance law is revealed to support practical applications. Numerical simulations clearly demonstrate the effectiveness of the proposed formulation.

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