FIELD: navigation.
SUBSTANCE: invention relates to the field of aircraft planes navigation using compound method of navigation, functionally combining inertial method of navigation, satellite way of navigation and air-speed way of navigation, and also relates to the navigators for the control and management of aircraft planes. Proposed small-sized navigation system contains a satellite navigation system (SNS) receiver, an integrated sensor box, air signal system (ASS), three-component magnetometric sensor (MS), limit switch of strut compression, cluster for determining the reliability of SNS signals, a computing section, range unit of deviation ratio of MS, range unit of heading of aircraft, cluster of reserve navigation, adaptation unit to bumpiness.
EFFECT: technical result achieved at implementation of the proposed device, is to reduce the time of initial exhibition, increase reliability and increase the accuracy of determining the true track.
1 cl, 1 tbl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMPLEX METHOD OF AIRCRAFT NAVIGATION | 2016 |
|
RU2646957C1 |
| SMALL-SIZE ADAPTIVE ATTITUDE-AND-HEADING REFERENCE SYSTEM | 2016 |
|
RU2714144C2 |
| SELF-ORGANIZING NAVIGATION COMPLEX | 2016 |
|
RU2640964C1 |
| METHOD OF DETERMINING ANGLES OF SPATIAL ORIENTATION | 2016 |
|
RU2713078C1 |
| PLATFORMLESS INS ORIENTATION ANGLES CORRECTION METHOD | 2022 |
|
RU2796328C1 |
| ADAPTIVE ATTITUDE ANGLE CORRECTOR FOR STRAPDOWN INERTIAL NAVIGATION SYSTEM | 2020 |
|
RU2749152C1 |
| ADAPTIVE STRAP DOWN INERTIAL ATTITUDE-AND-HEADING REFERENCE SYSTEM | 2016 |
|
RU2647205C2 |
| METHOD OF CORRECTION OF PLATFORM-FREE INERTIAL NAVIGATION SYSTEM | 2016 |
|
RU2635820C1 |
| STRAP DOWN INERTIAL ATTITUDE-AND-HEADING REFERENCE | 2016 |
|
RU2643201C2 |
| SMALL-SIZE PLATFORMLESS INERTIAL NAVIGATION SYSTEM OF MEDIUM ACCURACY, CORRECTED FROM SYSTEM OF AIR SIGNALS | 2012 |
|
RU2502049C1 |
