The effectiveness of pole placement method in control system design for an autonomous helicopter model in hovering flight
This paper presents the results of attitude, velocity, heave and yaw controller design for an autonomous model scaled helicopter using identified model of vehicle dynamic from parameterized state-space model with quasi-steady attitude dynamic approximation (6 Degree of Freedom model). Multivariable...
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| வடிவமà¯: | கடà¯à®Ÿà¯à®°à¯ˆ |
| வெளியீடபà¯à®ªà®Ÿà¯à®Ÿà®¤à¯: |
Penerbit Universiti Tun Hussein Onn Malaysia
2011
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| பகà¯à®¤à®¿à®•à®³à¯: | |
| நிகழà¯à®¨à®¿à®²à¯ˆ அணà¯à®•à®²à¯: | http://penerbit.uthm.edu.my/ejournal/ http://penerbit.uthm.edu.my/ejournal/ http://eprints.uthm.edu.my/508/1/6._Prof_Abas_F.pdf |
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