FIELD: physics.
SUBSTANCE: group of inventions relates to the device of receiving navigation signals, the multi-mode receiver to facilitate the navigation of an aircraft, the hybrid system to facilitate the navigation. The device for receiving radio-navigation signals comprises two GNSS modules, each of which comprises a radio-navigation signal processing means, a guidance data calculating means and a data comparing means of the both modules. The multi-mode receiver, facilitating navigation of an aircraft, includes the instrument landing system ILS and the radio-navigation signal receiving device. The hybrid system includes a multi-mode receiver with the instrument landing system ILS with the hybridization inertial system GNSS-IRS, where IRS - the inertial system and GNSS - the means of the navigation data hybridization, a radio-navigation signal receiving device.
EFFECT: precision landing and automatic steering an aircraft in poor visibility conditions.
14 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT VERTICAL-PLANE GUIDANCE FINAL APPROACH INSTRUMENT | 2006 |
|
RU2362976C1 |
| NEAR-FIELD NAVIGATION SYSTEM | 2012 |
|
RU2602833C2 |
| METHOD OF DETERMINING POSITION OF MOVING OBJECT AT GIVEN MOMENT AND MONITORING ACCURACY OF POSITION OF SAID MOVING OBJECT | 2010 |
|
RU2513551C2 |
| AIRCRAFT LANDING SYSTEM | 2023 |
|
RU2809110C1 |
| AIRCRAFT LANDING DEVICE | 2020 |
|
RU2757804C1 |
| HELICOPTER ONBOARD EQUIPMENT COMPLEX BASED ON INTEGRATED MODULAR AVIONICS | 2015 |
|
RU2605222C1 |
| METHOD AND SYSTEM FOR PREDICTING PERFORMANCE OF SATELLITE NAVIGATION SYSTEMS | 2008 |
|
RU2467352C2 |
| VALIDITY CONTROL METHOD AND COMBINATION/CONSOLIDATION DEVICE WITH MULTIPLE PROCESSING MODULES | 2014 |
|
RU2634693C2 |
| METHOD OF AIRCRAFTS LANDING USING SATELLITE NAVIGATION SYSTEM AND SATELLITE-BASED LANDING SYSTEMS | 2007 |
|
RU2331901C1 |
| AIRCRAFT MULTI-POSITION LANDING SYSTEM | 2019 |
|
RU2717284C2 |
