Integrated Guidance and Control Using Model Predictive Control with Flight Path Angle Prediction against Pull-Up Maneuvering Target

Integrated guidance and control using model predictive control against a maneuvering target is proposed. Equations of motion for terminal homing are developed with the consideration of short-period dynamics as well as actuator dynamics of a missile. The convex optimization problem is solved consider...

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Detalles Bibliográficos
Autores principales: Park, Jongho, Kim, Youngil, Kim, Jong-Han
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7313701/
https://www.ncbi.nlm.nih.gov/pubmed/32498281
http://dx.doi.org/10.3390/s20113143

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7313701/
https://www.ncbi.nlm.nih.gov/pubmed/32498281
http://dx.doi.org/10.3390/s20113143

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