Development of the algorithm for aircraft control at inaccurate measurement of the state vector and variable accuracy parameter
A parametric method of the synthesis of control in the closed circuit, taking into account explicitly generalized error of the inertial module, is presented. The law of control in the form of analytical formulas is typically assigned to the control program and does not change during flight of an unm...
| Main Authors: | , , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
PC Technology Center
2018-02-01
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| Series: | Eastern-European Journal of Enterprise Technologies |
| Subjects: | |
| Online Access: | http://journals.uran.ua/eejet/article/view/123271 |