Sangam: A Confluence of Knowledge Streams

Optimal impact angle guidance for exo-atmospheric interception utilizing gravitational effect

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dc.creator He, Shaoming
dc.creator Lee, Chang-Hun
dc.date 2018-09-26T11:43:46Z
dc.date 2018-09-26T11:43:46Z
dc.date 2018-09-24
dc.date.accessioned 2022-05-25T16:38:33Z
dc.date.available 2022-05-25T16:38:33Z
dc.identifier Shaoming He and Chang-Hun Lee. Optimal impact angle guidance for exo-atmospheric interception utilizing gravitational effect. IEEE Transactions on Aerospace and Electronic Systems, Volume 55, Issue 3, 2019, pp. 1382-1392
dc.identifier 0018-9251
dc.identifier https://doi.org/10.1109/TAES.2018.2870456
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/13493
dc.identifier.uri http://localhost:8080/xmlui/handle/CUHPOERS/182349
dc.description This paper aims to develop a new optimal intercept angle guidance law for exo-atmospheric interception by utilizing gravity. A finite-time optimal regulation problem is formulated by considering the instantaneous zero-effort-miss (ZEM) and the intercept angle error as the system states. The analytical guidance command is then derived based on Schwarz's inequality approach and Lagrange multiplier concept. Capturability analysis using instantaneous linear time-invariant system concept is also presented to provide better insights of the proposed guidance law. Theoretical analysis reveals that the proposed optimal guidance law encompasses previously suggested optimal impact angle constrained guidance laws. Numerical simulations with some comparisons clearly demonstrate the effectiveness of the proposed guidance law.
dc.language en
dc.publisher IEEE
dc.rights Attribution-NonCommercial 4.0 International
dc.rights http://creativecommons.org/licenses/by-nc/4.0/
dc.subject Missile guidance
dc.subject Intercept angle
dc.subject Optimal control
dc.subject Varying-speed
dc.subject Gravity
dc.title Optimal impact angle guidance for exo-atmospheric interception utilizing gravitational effect
dc.type Article


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