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Aerospace Instrument-Making Annotation << Back
Peculiarities of the aircraft control system drive dynamics in the case of stretched airframes and the uses of linear accelerometers signals |
В. V. Viktorov, V.D. Eliseev
Peculiarities of the aircraft (airplane, rocket and so on) control system drive dynamics of its own is under investigation in the case of the uses of linear accelerometers signals. Positions of these sensors axises of sensitivity are normal to the aircraft axis of bank. It was demonstrated that the drive mechanism inherent stability loss is possible in the case of the specific placement of sensors along the aircraft axis of bank. The loss of the drive mechanism inherent stability is associated with the change in the reduced static characteristics. The general case of the problem taking into account the airframe elasticity is considered. Recommendations with respect to the uses of these results were fixed. |
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