| 摘要 |
FIELD: aviation electronics, systems of stability and controllability of aircraft. SUBSTANCE: salient feature of proposed system lies in usage of combined electric circuit in computer, analog and digital, simplified and convenient adjustment of transmission coefficients of paths of roll, pitch and course by reprogramming of proper working registers of computer, insertion of cross couplings between control channels to simplify control laws of computer. EFFECT: increased efficiency of utilization of electric remote control system, diminished mass and size characteristics and consumed power. 5 dwg |
