FIELD: aircraft engineering.
SUBSTANCE: identification is performed at relatively simple test signal without whatever a priori assumptions relative to the characters of nonlinearity of identified single-valued aerodynamic characteristic. Elimination of errors of a priori assumptions about the character of nonlinearity of identified relationships allows the increase in validity of determination of nonlinear aerodynamic characteristics in flight tests.
EFFECT: higher validity and accuracy of determination of flight test nonlinear aerodynamic characteristics.
5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND SYSTEM FOR CONTROLLING LONGITUDINAL MOVEMENT DURING TAKEOFF ON FLIGHT STRIP AND CLIMBING OF UNMANNED AERIAL VEHICLE WITH SPECIALLY ARRANGED FRONT AND REAR WINGS | 2018 |
|
RU2695897C1 |
| METHOD OF DETERMINING AIRCRAFT AERODYNAMIC ANGLE | 2007 |
|
RU2341775C1 |
| METHOD OF AIRCRAFT ENGINE THRUST DETERMINING AT OPERATING MODE CHANGE AND DEVICE FOR ITS IMPLEMENTATION | 2015 |
|
RU2601367C1 |
| COURSE CHANNEL AIRCRAFT CONTROL SYSTEM | 2021 |
|
RU2768310C1 |
| METHOD OF IDENTIFICATION OF AERODYNAMIC CHARACTERISTICS OF AUTOMATICALLY CONTROLLED FLIGHT VEHICLES | 1994 |
|
RU2124711C1 |
| METHOD OF DETERMINING AERODYNAMIC CHARACTERISTICS OF AIRCRAFT | 2011 |
|
RU2460982C1 |
| METHOD FOR GENERATING ADAPTIVE ANGULAR STABILIZATION SIGNAL BASED ON AIRCRAFT ROLL | 2023 |
|
RU2809632C1 |
| SYSTEM OF AUTOMATED MODAL CONTROL IN AIRCRAFT LONGITUDINAL AXIS | 2015 |
|
RU2644842C2 |
| METHOD OF IDENTIFYING AIRCRAFT AERODYNAMIC CHARACTERISTICS BY TEST RESULTS | 2009 |
|
RU2419775C1 |
| METHOD FOR DETERMINATION OF ATTACK AND SLIP ANGLES OF UNMANNED AERIAL VEHICLE | 2022 |
|
RU2792261C1 |
