FIELD: aircraft engineering.
SUBSTANCE: proposed system comprises navigation measurement complex, first and second scaling units, fur adders, two nonlinear units, integrator, signal multiplication unit, lengthwise control overload ACS, elevator and steering drive. Inputs of nonlinear unit and inputs of the second and fourth adders are connected to outputs of navigation and measurement complex. Output of the first nonlinear unit is connected to inputs of the first scaling unit, second nonlinear unit and third adder input. Integrator, second adder and first signal multiplication unit are connected to third adder. Second nonlinear unit and fourth adder are connected to signal multiplication first unit, fourth adder output being connected to second input of scaling unit. Integrator input is connected to second adder output. First adder output is connected to input of lengthwise control overload ACS.
EFFECT: ruled out parallel drift from approach path.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT AUTOMATIC CONTROL SYSTEM WITH REDUCTION OF CIRCLE HEIGHT AT STABILIZATION STAGE | 2018 |
|
RU2703378C1 |
| METHOD OF AIRCRAFT CONTROL IN LANDING APPROACH | 2012 |
|
RU2537201C2 |
| SYSTEM OF AUTOMATIC CONTROL OF THE AIRCRAFT AT THE CLIMB AND STABILIZATION OF THE TOTAL HEIGHT OF THE FLIGHT | 2016 |
|
RU2619793C1 |
| AIRCRAFT SIDE MOVEMENT AT LANDING APPROACH AUTOMATIC CONTROL SYSTEM | 2017 |
|
RU2662576C1 |
| METHOD FOR PLANE CONTROL WHEN RETURNING TO AIRFIELD UNDER FUEL-SAVING CONDITIONS | 2020 |
|
RU2749167C1 |
| CONTROL SIGNAL GENERATOR FOR DESCENT CONDITIONS | 2010 |
|
RU2439499C1 |
| CONTROL SYSTEM IN LONGITUDINAL CHANNEL OF MANNED AND UNMANNED AIRCRAFTS IN MODE OF CREEPING FROM DANGEROUS HEIGHT AT WORK ON GROUND OBJECTS | 2016 |
|
RU2644048C2 |
| MANNED AIRCRAFT CONTROL SYSTEM WITH ADAPTIVE CROSS LINK | 2019 |
|
RU2736400C1 |
| LIMITER OF MANEUVERABLE AIRCRAFT LIMIT MODES OF FLIGHT | 2019 |
|
RU2711040C1 |
| INTELLIGENT SYSTEM OF CREW SUPPORT | 2013 |
|
RU2541902C2 |
