RU95119669A - METHOD OF MEASUREMENT - Google Patents

METHOD OF MEASUREMENT

Info

Publication number
RU95119669A
RU95119669A RU95119669/28A RU95119669A RU95119669A RU 95119669 A RU95119669 A RU 95119669A RU 95119669/28 A RU95119669/28 A RU 95119669/28A RU 95119669 A RU95119669 A RU 95119669A RU 95119669 A RU95119669 A RU 95119669A
Authority
RU
Russia
Prior art keywords
helmet
inertial
inertial system
directed
axis
Prior art date
Application number
RU95119669/28A
Other languages
Russian (ru)
Other versions
RU2117250C1 (en
Inventor
К.М. Лучанский
В.Ф. Левитин
Н.Т. Лоповок
Original Assignee
Государственный научно-исследовательский институт авиационных систем
Filing date
Publication date
Application filed by Государственный научно-исследовательский институт авиационных систем filed Critical Государственный научно-исследовательский институт авиационных систем
Priority to RU95119669/28A priority Critical patent/RU2117250C1/en
Priority claimed from RU95119669/28A external-priority patent/RU2117250C1/en
Publication of RU95119669A publication Critical patent/RU95119669A/en
Application granted granted Critical
Publication of RU2117250C1 publication Critical patent/RU2117250C1/en

Links

Claims (1)

Способ измерения, включающий определение положения шлема оператора относительно осей координат, отличающийся тем, что на шлеме устанавливают инерциальную систему, осуществляют выставку осей координат этой инерциальной системы в соответствии с начальным положением шлема и измеряют абсолютные координаты шлема оператора, например, по месту установки инерциальной системы, причем за начало координат инерциальной системы принимают, например, центр масс этой системы в момент выставки, при этом ортогональные оси OX, OY инерциальной системы координат направляют в горизонтальной плоскости, причем ось OX направляют на Север, а ось OZ инерциальной системы координат ориентируют по местной вертикали.A measurement method, including determining the position of the helmet of the operator relative to the coordinate axes, characterized in that an inertial system is mounted on the helmet, the coordinate axes of this inertial system are set in accordance with the initial position of the helmet, and the absolute coordinates of the helmet of the operator are measured, for example, at the installation site of the inertial system, moreover, the origin of coordinates of the inertial system is taken, for example, the center of mass of this system at the time of the exhibition, while the orthogonal axes OX, OY of the inertial system rdinat directed in a horizontal plane, the OX axis is directed to the north, and the OZ axis of the inertial coordinate system oriented along the local vertical.
RU95119669/28A 1995-11-21 1995-11-21 Method of measurement RU2117250C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95119669/28A RU2117250C1 (en) 1995-11-21 1995-11-21 Method of measurement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95119669/28A RU2117250C1 (en) 1995-11-21 1995-11-21 Method of measurement

Publications (2)

Publication Number Publication Date
RU95119669A true RU95119669A (en) 1997-10-27
RU2117250C1 RU2117250C1 (en) 1998-08-10

Family

ID=20173997

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95119669/28A RU2117250C1 (en) 1995-11-21 1995-11-21 Method of measurement

Country Status (1)

Country Link
RU (1) RU2117250C1 (en)

Similar Documents

Publication Publication Date Title
CA2269957A1 (en) Automated guided apparatus suitable for toping applications
NO913994L (en) POINT MEASUREMENT OF SPACIAL COORDINATES
DE69108220D1 (en) Device for tracking transient seismic signals along orthogonal axes.
DE69621669D1 (en) Three-dimensional coordinate measuring machine
FR2702043B1 (en) Three-dimensional coordinate measuring machines.
DE69412216D1 (en) System for determining acceleration using a gravity accelerometer with zero point adjustment
DE60004063D1 (en) BODENNAVIGATIONSGERAET
FR2601460B1 (en) INSTALLATION FOR THE DETECTION AND LOCATION OF SPACE BY INTERFEROMETRIC MEASUREMENT, IN REAL TIME AND AT LARGE DISTANCE
CA2212925A1 (en) Method to determine local variations of the earth's magnetic field and location of the source thereof
DE3676349D1 (en) SYSTEM FOR PRESENTING INFORMATION.
EP1207403A4 (en) Method for determining the position of reference axes in an inertial navigation system of an object in respect with the basic coordinates and embodiments thereof
RU95119669A (en) METHOD OF MEASUREMENT
DE69319637D1 (en) Display for the coordinate system guidance of an NC device
JO1611B1 (en) Universal map display system, in paticular of visualisation on an object whose position is identified using any coordinate system
KR910700511A (en) Navigation system combining map
FR2551890B1 (en) SPATIAL FIELD ANALYSIS DEVICE FOR THE ANGULAR LOCATION OF RADIANT OBJECTS
DE4447905B4 (en) Coordinate measuring machine for measuring three-dimensional coordinates
IT9047561A0 (en) NAVIGATION SYSTEM AND METHOD FOR DETERMINING THE RELATIVE POSITIONS OF TWO OBJECTS
SU1698637A1 (en) Device for localization in fixing element space
RU93012818A (en) METHOD FOR DETERMINING GEOGRAPHIC COORDINATES OF AN OBJECT
UA30187A (en) РПаЎ±б
SU532812A1 (en) Device for determining the coordinates of defects in linear objects
SU878608A1 (en) Device for drawing perspective
RU95112881A (en) METHOD FOR PRODUCING NAVIGATION PARAMETERS AND VERTICAL LOCATIONS
RU97102442A (en) METHOD FOR PRODUCING NAVIGATION PARAMETERS AND VERTICAL LOCATIONS