Aircraft lateral-directional control without a roll command in the autopilot

The laws of lateral motion control without data on the roll angle are proposed for aircraft with a single plane of symmetry. A procedure for analytical selection of the optimal gain in the aileron and rudder channels is proposed. The results of simulating the aircraft-autopilot system are presented.

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Bibliographic Details
Published in:Russian aeronautics 2014-04, Vol.57 (2), p.134-140
Main Authors: Romanenko, L. G., Samarova, G. G., Romanenko, A. G.
Format: Article
Language:English
Subjects:
Aircraft
Automotive Engineering
Channels
Engineering
Flight Dynamics and Control of Flight Vehicles
Gain
Mathematical analysis
Optimization
Rolls
Simulation
Symmetry
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Description
Summary:The laws of lateral motion control without data on the roll angle are proposed for aircraft with a single plane of symmetry. A procedure for analytical selection of the optimal gain in the aileron and rudder channels is proposed. The results of simulating the aircraft-autopilot system are presented.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799814020044