FIELD: instrument making.
SUBSTANCE: they combine a process of initial setting of an inertial navigation system (INS) and a process of steering to a landing strip (LS). At the same initial setting of INS is started in the mode of ground setting, and immediately after achievement of minimum sufficient characteristics of INS they start taking off an aircraft (AC), continuing initial setting of INS in the mode of setting on board. The full set of parameters sent to the inlet of INS when set on board is determined with the help of the INS itself and a satellite navigation system (SNS) of the AC and replaced at the inlet of INS. In case of SNS failure or no data after start of AC takeoff the initial setting of INS is continued only during possible stops of AC, stopping it during AC movement.
EFFECT: expanded functional capabilities.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT COMPLEX PREPARATION AND NAVIGATION SYSTEM | 2010 |
|
RU2434202C1 |
| UNIFIED AIRCRAFT NAVIGATION SYSTEM | 2015 |
|
RU2590934C1 |
| CONTROL OVER AIRCRAFT LANDING PATH AT LANDING ON NONPROGRAMMED AIRFIELD | 2013 |
|
RU2546550C1 |
| METHOD OF CONTROL OF AIRCRAFT LANDING PATH AT LANDING ON PROGRAMMED AIRFIELD | 2013 |
|
RU2549145C1 |
| SMALL-SIZED NAVIGATIONAL COMPLEX | 2016 |
|
RU2644632C1 |
| METHOD FOR DETERMINING OBJECT ORIENTATION PARAMETERS USING SEMI-ANALYTICAL INERTIAL NAVIGATION SYSTEM WITH GEOGRAPHICAL ORIENTATION OF FOUR-AXIS GYROPLATFORM AXES | 2022 |
|
RU2782334C1 |
| METHOD OF INCREASING ACCURACY OF INITIAL ALIGNMENT OF STRAPDOWN INERTIAL SYSTEM | 2015 |
|
RU2591738C1 |
| METHOD OF MEASUREMENT OF COURSE OF AIRCRAFT | 2000 |
|
RU2178145C1 |
| METHOD OF INERTIAL DATA ESTIMATION AND ITS CORRECTION ACCORDING TO MEASUREMENT OF SATELLITE NAVIGATION SYSTEM | 2015 |
|
RU2617565C1 |
| METHOD OF ALIGNMENT OF PINS AC OF SHIP BASE AND DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2635398C2 |
