FIELD: aircraft engineering.
SUBSTANCE: group of inventions relates to a method and a device for forming an aircraft flight path. To form an aircraft flight path signals are transmitted to a memory unit proportional to coordinates, heading and horizontal speed of the target, they are saved for the reception moment, then a given miss value is transmitted or entered, the obtained signals are compared, the aircraft deviations by heading and range are evaluated, a correction to the current heading is received, saved in the output buffer and transmitted from the buffer to the aircraft heading automatic control system to be worked out, the aircraft movement as per the specified radius around the target is provided, a new flight path considering the target motion is formed. Device for forming a flight path comprises a switch, a memory unit, two subtractors, an output buffer, a range unit, a false target unit, an angular shift unit, a logical unit - all interconnected in a certain manner. False target unit comprises two dividers, an arcsine calculator, an arctangent calculator, a comparator, a multiplier, two arithmetic devices. Angular shift unit comprises two sinus calculators, two multipliers, a subtractor. Logical unit comprises two units of comparison with a preset value, an amplifier, two subtractors, five multipliers, two dividers, two inverters, an arctangent calculator, two adders.
EFFECT: provided is automatic forming the aircraft flight path at the target movement.
5 cl, 8 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR FUNCTIONING OF MISSILE INFORMATION-COMPUTING SYSTEM AT GUIDANCE TO TARGET AND DEVICE FOR ITS REALIZATION | 2006 |
|
RU2311605C2 |
SIMULATOR COMPLEX FOR CHECKING CONTROL SYSTEM OF UNMANNED AIRCRAFT | 2010 |
|
RU2432592C1 |
SYSTEM FOR PREDICTING UNMANNED AIRCRAFT FULL-SCALE TEST RESULTS | 2000 |
|
RU2160927C1 |
SYSTEM FOR PREDICTION OF FUEL-SCALE TEST RESULTS OF UNMANNED AIRCRAFT | 2000 |
|
RU2163732C1 |
MODE OF FUNCTIONING OF DATA-PROCESSING SYSTEMS OF ROCKET AND ARRANGEMENT FOR ITS EXECUTION | 2004 |
|
RU2292523C2 |
METHOD AND DEVICE FOR FORMING OF ON-BOARD GUIDANCE TRAJECTORY | 1994 |
|
RU2136034C1 |
METHOD OF FUNCTIONING OF INFORMATION COMPUTATION SYSTEM OF MISSILE AND DEVICE THEREFOR | 2007 |
|
RU2332634C1 |
METHOD OPERATING MISSILE DATA PROCESSING SYSTEM AND DEVICE TO THIS END | 2007 |
|
RU2351889C2 |
METHOD FOR FUNCTIONING OF MISSILE INFORMATION-COMPUTER SYSTEM AND DEVICE FOR ITS REALIZATION | 2004 |
|
RU2253825C1 |
SYSTEM FOR DETERMINATION OF COORDINATES OF SEAPLANE POSITION ON SEA SURFACE | 1990 |
|
RU1797300C |
Authors
Dates
2016-09-10—Published
2015-07-20—Filed