FIELD: aviation. SUBSTANCE: invention refers to pilotage-navigation complexes of flying vehicles. Approximate value of angle of sideslip is determined by data on values of angles of roll and course, on moduli of ground 1,4,5 and air 2 speeds and by data on modulus and direction 16 of wind in computer 8 which increases sufficiency accuracy of reckoning of navigational parameters. EFFECT: increased accuracy of coordinate reckoning and improved characteristics of stability of flying vehicle if Doppler speedometer fails. 2 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMMAND-AND-FLIGHT INDICATOR | 2019 |
|
RU2716886C1 |
| COMPLEX COURSE SYSTEM | 1993 |
|
RU2077029C1 |
| METHOD OF CONTROL OF THE PILOTAGE-NAVIGATION COMPLEX AND DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2658538C2 |
| METHOD AND APPARATUS FOR CONTROLLING PILOT-NAVIGATION SYSTEM | 2010 |
|
RU2440595C1 |
| FLIGHT DIRECTOR INDICATOR OF A HELICOPTER | 2021 |
|
RU2778955C1 |
| FLIGHT DIRECTOR DISPLAY | 2018 |
|
RU2711196C1 |
| DEVICE FOR DETERMINING ERROR OF MEASUREMENT OF ANGLES OF ATTACK AND GLIDING | 2014 |
|
RU2579551C1 |
| SYSTEM FOR CONTROL OF FLIGHT-NAVIGATION COMPLEX | 2009 |
|
RU2393429C1 |
| MODE OF CALIBRATION OF A SENSOR OF AN AERODYNAMIC ANGLE OF A FLYING VEHICLE | 2004 |
|
RU2277698C1 |
| METHOD AND DEVICE FOR CONTROLLING HORIZONTAL ORIENTATION OF AIRCRAFT | 2007 |
|
RU2373562C2 |
