Adaptation of pendulum correction of an aircraft strapdown gyrovertical to flight conditions
| Autor: | V. S. Kulabukhov, B. O. Kachanov, S. K. Akhmedova, N. A. Tuktarev, D. V. Grishin |
|---|---|
| Rok vydání: | 2017 |
| Předmět: |
Engineering
General Computer Science business.industry Attitude and heading reference system Pendulum ComputerApplications_COMPUTERSINOTHERSYSTEMS Gyroscope Mechatronics Flight simulator Fly-by-wire law.invention Hardware_GENERAL Control and Systems Engineering law Inertial measurement unit Electrical and Electronic Engineering Aerospace engineering business Flight control modes Physics::Atmospheric and Oceanic Physics |
| Zdroj: | Gyroscopy and Navigation. 8:115-120 |
| ISSN: | 2075-1109 2075-1087 |
| DOI: | 10.1134/s2075108717020067 |
| Popis: | An algorithm for a gyrovertical based on MEMS sensors for detecting pitch and roll angles of aircraft is considered. It is suggested to integrate inertial sensors with an air data system. A flight simulator is used to optimize the algorithm coefficients. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
|
Full text from SpringerLink