Parameter design for a guidance and control system using genetic approach

DOI10.1016/S1270-9638(01)01121-XzbMath1004.93037OpenAlexW1969376115MaRDI QIDQ2778687

Rei-Min Lai, Chun-Liang Lin

Publication date: 2 February 2003

Published in: Aerospace Science and Technology (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s1270-9638(01)01121-x

zbMATH Keywords

optimal controlgenetic algorithmguided missilegenetic searchenergy consumptionstability constraintproportional navigationaerodynamic turning rate time constantfinal miss distanceguidance filter time constant

Mathematics Subject Classification ID

Application models in control theory (93C95) Design techniques (robust design, computer-aided design, etc.) (93B51)

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