FIELD: measurement equipment.
SUBSTANCE: linear speed of an aircraft is determined through projections of its vector to horizontal and vertical planes. At each k time moment there used is data that is supplied from a television system included in an optic electronic system and from a thermal direction finder included in the optic electronic system. Besides, current values of yawing angles of the aircraft and pitching angles of the aircraft are used at k and (k-1) time moments respectively. Angular speed of the change of the aircraft yawing angle ωψk and angular speed of the change of the aircraft pitching angle ωϑk at k time moment is determined.
EFFECT: improving measurement accuracy of linear speed of an aircraft using non-radar information.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR CONTROLLING POSITION OF ANTENNA AXIS OF ON-BOARD RADAR STATION WHEN ACCOMPANYING MANEUVERING AERIAL TARGET | 2020 |
|
RU2758446C1 |
| METHOD FOR DETERMINATION OF RANGE TO SOURCES OF RADIO EMISSION AND RATE OF CLOSURE TO THEM IN SINGLE-POSITION RADAR SYSTEMS | 2002 |
|
RU2232402C2 |
| METHOD OF DETERMINING SPATIAL ORIENTATION ANGLES OF AIRCRAFT AND DEVICE THEREFOR | 2015 |
|
RU2594631C1 |
| INERTIAL RADIO NAVIGATION SYSTEM | 2013 |
|
RU2539846C1 |
| METHOD OF DETERMINING SPATIAL ORIENTATION ANGLES OF AIRCRAFT AND DEVICE THEREFOR | 2015 |
|
RU2589495C1 |
| METHOD OF DETERMINING BANKING ANGLE OF BANKING AIRCRAFT | 2013 |
|
RU2527369C1 |
| METHOD OF DETERMINATING OF DISTANCE UP TO MANEUVERABLE AIRCRAFT IN NO-SIGNAL CONDITION OF RADAR STATION ON BASIS OF USAGE OF NON-RADIOLOCATING INFORMATION | 2008 |
|
RU2363016C1 |
| METHOD OF DETERMINING COORDINATES OF RADIO-FREQUENCY RADIATION SOURCE ONBOARD AIRCRAFT | 2012 |
|
RU2510618C2 |
| DEVICE TO DETECT ANGLES OF SPATIAL ORIENTATION OF MOVABLE OBJECT | 2014 |
|
RU2555496C1 |
| IMAGE SHIFT COMPENSATION METHOD | 1991 |
|
RU2018894C1 |
