Сontrol system for a light-duty aerospace rocket complex based on a platformless inertial navigation system

Author:

Kamelin A.B.,

Publisher

National Academy of Sciences of Ukraine (Co. LTD Ukrinformnauka)

Subject

Anesthesiology and Pain Medicine

Reference8 articles.

1. 1. Aerodynamic missile system of light class [Ajerodinamicheskij raketnyj kompleks legkogo klassa]. Materialy AP, pt. II. Sistema upravlenija, 20 p. (AO Avionika, Kiev, 1995) [in Russian].

2. 2. Grechka G. P., Kamelin A. B. Characteristics of Laser gyroscopes from the point of view of the requirements of FINOS [Harakteristiki LG s tochki zrenija trebovanij BINS]. Free inertial navigation and orientation systems [Besplatformennye inercial'nye sistemy navigacii i orientacii], Shkola-87, kn. 2 (AN SSSR, Moscow, 1989) [in Russian].

3. Status of and trends of cardanless aircraft inertial navigation systems;Zlatkin;Mechanics of Gyroscopic Systems Is,1997

4. Complex construction of the system. Computing tools and software-algorithmic support of FINOS [Kompleksnoe postroenie sistemy. Vychislitel'nye sredstva i programmno-algoritmicheskoe obespechenie BINS.,1995

5. 5. Lukyanov D. P. (Ed.) Laser Measuring Systems, 259 p. (Radio i svyaz, Moscow, 1981) [in Russian].

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