The problem of synthesizing the pitch angle control system with the angle of attack limiting channel is considered. The problem of matching the trajectories of the system of the pitch angle control mode and the angle of attack limitation mode is discussed. An approach is proposed based on using a generalized characteristic of the system, which ensures the matching the states at an arbitrary moment of change of its operation mode.
Synthesis of Pitch Angle Control System with Angle of Attack Limiting Channel
Russ. Aeronaut.
Russian Aeronautics ; 63 , 1 ; 25-32
2020-01-01
8 pages
Article (Journal)
Electronic Resource
English
AIRCRAFT PITCH ANGLE AND LIMITING PARAMETERS AUTOMATIC CONTROL SYSTEM
European Patent Office | 2015
|PITCH ANGLE CONTROL SYSTEM, PITCH ANGLE CONTROL METHOD, AND VEHICLE
European Patent Office | 2018
|PITCH ANGLE CONTROL SYSTEM, PITCH ANGLE CONTROL METHOD, AND VEHICLE
European Patent Office | 2015
|AUTOMATIC CONTROL SYSTEM OF PITCH ANGLE AND LIMITATION OF ANGLE OF ATTACK OF AIRCRAFT
European Patent Office | 2019
|Roll-pitch-yaw integrated μ-synthesis for high angle-of-attack missiles
Elsevier | 2011
|