Hammer-head turn flight control of helicopters by using a thrust selection / desired attitude calculation based on a loading trajectory and a threshold
The design method for reference trajectory calculation and flight control system development of the autonomous hammer-head turn maneuver and verification results applied to unmanned helicopters are described. The whole maneuver is divided into four processes. Polynomial of the load factor is formula...
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| Format: | Article |
| Language: | Japanese |
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The Japan Society of Mechanical Engineers
2021-08-01
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| Series: | Nihon Kikai Gakkai ronbunshu |
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| Online Access: | https://www.jstage.jst.go.jp/article/transjsme/87/900/87_21-00170/_pdf/-char/en |