Abstract
The essence of direct force/aerodynamic force compound control is to improve the maneuverability and rapidity of controlled aircraft by using the fast response speed of direct force, which can effectively compensate the slow response of aerodynamic control caused by insufficient aerodynamic force. This paper describes the characteristics and key problems of direct force/aerodynamic force compound control system, and introduces the modeling method of direct force/aerodynamic force compound control system from three aspects: the configuration of engine, the existing research of direct force modeling at home and abroad, and the disturbance modeling of direct force control.The direct force/aerodynamic force compound control method is introduced from three aspects: the control method, the existing research of direct force/aerodynamic force compound control method at home and abroad, and the ignition algorithm of pulse engine. The feasible direct force/aerodynamic force compound system stability analysis method is given, the future development trend of direct force/aerodynamic force compound control is prospected, and its key technologies are summarized.
| Translated title of the contribution | Review on Development of Direct Force/Aerodynamic Force Compound Control Technology |
|---|---|
| Original language | Chinese (Traditional) |
| Pages (from-to) | 1-13 |
| Number of pages | 13 |
| Journal | Aero Weaponry |
| Volume | 29 |
| Issue number | 1 |
| DOIs | |
| State | Published - 28 Feb 2022 |