Longitudinal Absolute Stability of a BWB Aircraft-Pilot System with Saturated Actuator Model
This paper deals with the analysis of the P(ilot) I(n-the-Loop) O(scillations) of the second category (with rate and position liming in the closed loop pilot-vehicle system), caused by the dynamic coupling between the human pilot and the aircraft. The analysis is made in the context of the longitudi...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2013-09-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/state_c_a__v5_iss_3_full.pdf |