INERTIAL SATELLITE NAVIGATION SYSTEM Russian patent published in 2000 - IPC

Abstract RU 2148796 C1

FIELD: navigation systems. SUBSTANCE: goal of invention is achieved by removal of horizontal channels for controlling inertial navigation system gyros, and adding control signals from filters to output signals with respect to speed of horizontal channels. In addition, each horizontal channel of combined system has fourth and fifth adders and second integrator without feedback circuit, as well as unit for calculation of navigation parameters. EFFECT: increased precision, which is greater than standalone inertial navigation system and satellite navigation system receiver, continuous detection of current speed error of inertial navigation system, increased reliability due to removal of control signals to gyros, application for platform and strap-down navigation systems. 7 dwg

Similar patents RU2148796C1

Title	Year	Author	Number
INERTIAL SATELLITE NAVIGATION SYSTEM	2003	Volzhin A.S. Vjaz'Mikin A.A. Zinich V.S. Fal'Kov Eh.Ja.	RU2233431C1
METHOD OF INTEGRATION OF INTERNAL NAVIGATION SYSTEMS AND COMPLEX NAVIGATION SYSTEM	1993	Volzhin A.S. Ignatov A.I. Chervin V.I. Budkin V.L.	RU2082098C1
METHOD OF INTEGRATING NAVIGATION INFORMATION AND SELF-INTEGRATED INERTIAL NAVIGATION SYSTEM	2009	Volzhin Anatolij Sergeevich	RU2386108C1
COMPLEX NAVIGATION SYSTEM	2000	Nikulin A.S. Gerasimov G.I. Gorelov A.A. Dzhandzhgava G.I. Kolosov A.I. Kukolevskij O.I. Nikulina A.A. Orekhov M.I. Rogalev A.P. Semash A.A.	RU2178147C1
COMPLEX SYSTEM DETERMINING COURSE	2000	Nikulin A.S. Dzhandzhgava G.I. Kolosov A.I. Nikulina A.A. Orekhov M.I. Rogalev A.P. Shelepen' K.V.	RU2178146C1
METHOD OF MEASUREMENT OF COURSE OF AIRCRAFT	2000	Nikulin A.S. Dzhandzhgava G.I. Kolosov A.I. Nikulina A.A. Rogalev A.P. Shelepen' K.V. Aksinenko G.G.	RU2178145C1
AERIAL NAVIGATOR	2011	Dzhandzhgava Givi Ivlianovich Drozdov Aleksej Pavlovich Sazonova Tat'Jana Vladimirovna Trebukhov Andrej Viktorovich Shelagurova Marina Sergeevna	RU2457438C1
INERTIAL RADIO NAVIGATION SYSTEM	2013	Pjatkov Vjacheslav Viktorovich Meleshko Alla Vjacheslavovna Vasil'Ev Pavel Valer'Evich	RU2539846C1
METHOD AND SYSTEM TO GENERATE PARAMETERS OF ANGULAR ORIENTATION OF HULL	2014	Til' Anatolij Valentinovich	RU2573119C2
METHOD TO DETERMINE WIND SPEED ON BOARD OF AIRCRAFT AND DEVICE TO IMPLEMENT IT	2011	Nikulin Aleksandr Stepanovich Gerasimov Gennadij Ivanovich Dzhandzhgava Givi Ivlianovich Kavinskij Vladimir Valentinovich Negrikov Viktor Vasil'Evich Nikulina Anna Aleksandrovna Orekhov Mikhail Il'Ich Sukhorukov Sergej Jakovlevich	RU2486527C2

RU 2 148 796 C1

Authors

Bakhonin K.A.

Budkin V.L.

Volzhin A.S.

Dzhandzhgava G.I.

Prozorov A.S.

Dates

2000-05-10—Published

1998-11-05—Filed