FIELD: measurement equipment.
SUBSTANCE: method is based on use of information on fact of target localisation with a locator, the sensitivity axis of which coincides with direction of speed vector of the object. Trajectory of the object is formed in the form of cycles that begin and end by the fact of target localisation. Inside each cycle an arc-like movement is performed at maximum possible angular speed that is constant in the cycle, the sign of which is changed after achievement of the value of the average angle of advance of the object trajectory relative to a line of sighting, which is calculated for the current cycles as a product of difference of the value of this angle in the previous cycle and increase rate of the inclination angle of the object trajectory in the current cycle relative to the previous one multiplied by a coefficient depending on approach conditions, and a fraction, in the numerator of which there is difference of values of the average angle of advance in the previous cycle and rate of increase of the inclination angle of the object trajectory in the current cycle relative to the previous one, and in the denominator there is a sum of the specified values.
EFFECT: possible approach at opposite self-guidance when linear speed of the target exceeds speed of the object.
5 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF MOVING OBJECT HOMING BASING ON INFORMATION ON FACT OF TARGET SIGHTING AND DEVICE FOR ITS IMPLEMENTATION (VERSIONS) | 2014 |
|
RU2607758C2 |
MULTIFUNCTIONAL METHOD OF SELF-HOMING WITH DISCRETE CORRECTIONS OF TRAJECTORY | 2016 |
|
RU2623716C1 |
DEVICE FOR DETERMINING THE COORDINATES AND PARAMETERS OF MOTION OF THE OBSERVED FERROMAGNETIC OBJECT | 2021 |
|
RU2778326C1 |
METHOD FOR HOMING OF FLIGHT VEHICLES ON GROUND TARGETS | 1999 |
|
RU2164654C2 |
METHOD FOR PROPORTIONAL GUIDANCE OF FLIGHT VEHICLES ON GROUND OBJECTS | 1999 |
|
RU2148235C1 |
SELF-HOMING DEVICE | 2008 |
|
RU2392575C2 |
METHOD FOR FINAL REDUCTION OF AN UNMANNED AERIAL VEHICLE IN A LONGITUDINAL PLANE BASED ON A QUASI-OPTIMAL GUIDANCE LAW | 2020 |
|
RU2737840C2 |
METHOD TO CONTROL A GROUP OF UNMANNED AERIAL VEHICLES TAKING INTO ACCOUNT THE DEGREE OF DANGER OF SURROUNDING OBJECTS | 2019 |
|
RU2728197C1 |
METHOD OF CONTROLLING AND STABILISING MOBILE CARRIER, INTEGRATED SYSTEM, DEVICE FOR TURNING ANTENNA REFLECTOR IN TWO MUTUALLY-PERPENDICULAR PLANES AND DEVICE FOR ACTUATING DIFFERENTIAL AERODYNAMIC CONTROLLERS FOR REALISING SAID METHOD | 2009 |
|
RU2423658C2 |
MONOPULSE DETECTION AND HOMING RADAR SYSTEM | 2010 |
|
RU2439608C1 |
Authors
Dates
2015-06-10—Published
2014-05-05—Filed