| 摘要 |
FIELD: control of flying vehicle motion trajectory. ^ SUBSTANCE: proposed method consists in introducing preset acceleration, speed and coordinates into flying vehicle control system for obtaining the preset trajectory; during flight, deviation of present parameters from preset magnitudes are measured and total deviations in form of sums of said deviations and integral magnitudes of these deviations are determined. Control signals are formed from sums of deviations and their integral magnitudes. Device proposed for realization of this method includes navigational system unit 1, navigational information processing unit 2, automatic control unit 3 and manual control unit 4, shaping unit 5 and display unit 6. Shaping unit 5 has longitudinal, vertical and transversal channels. Transversal channel makes it possible to perform flat turn of flying vehicle in horizontal plane. Device may work in automatic, manual and combined modes. Automatic control may be corrected in flight, if required, by means of manual control without switching-off the automatic system. ^ EFFECT: enhanced accuracy; facilitated procedure of control; enhanced reliability of device. ^ 3 cl, 4 dwg |
