FIELD: trajectory setting method and device.
SUBSTANCE: inventions group relates to trajectory setting method and device. Trajectory is set the following way: set the target trajectory coordinate, calculate over the trajectory parameters, form the braking path reference, sum the current trajectory coordinate with the braking path reference and calculate the feedback coordinate, detect the trajectory braking section depending on the target trajectory coordinate, the initial trajectory coordinate and feedback coordinate, detect the trajectory setting completion. The device contains a trajectory target coordinate setter, two mismatch calculators, two relay regulators, a functional converter and an adder connected in a certain way.
EFFECT: invention provides for increasing a trajectory setting accuracy.
2 cl, 13 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR CONTROL OF SWITCHED RELUCTANCE MOTOR | 2019 |
|
RU2716129C1 |
METHOD OF AUTOMATIC REGULATION OF ELECTRIC DRIVE COORDINATE AND DEVICE FOR ITS IMPLEMENTATION | 2017 |
|
RU2660183C1 |
METHOD OF ADJUSTING PROPORTIONAL-INTEGRAL-DIFFERENTIAL CONTROLLER OF CLOSED DYNAMIC SYSTEM | 2019 |
|
RU2714372C1 |
METHOD OF THE INTERCONNECTED ELECTRIC DRIVES COORDINATES ADJUSTMENT | 2017 |
|
RU2655723C1 |
METHOD OF GUIDING AIRCRAFT TO GROUND TARGETS USING SYNTHETIC APERTURE RADAR | 2023 |
|
RU2824690C1 |
MULTICHANNEL REGULATTOR | 0 |
|
SU1532895A1 |
FLIGHT SIMULATION COMPLEX FOR INVESTIGATION OF LANDING SYSTEMS OF SHIP-BASED FLYING VEHICLES | 1991 |
|
RU2042583C1 |
METHOD FOR DETERMINATION OF AERODYNAMIC CHARACTERISTICS OF GUIDED MISSILE IN FLIGHT, METHOD FOR DETERMINATION OF ANGLE OF ATTACK OF MISSILE IN FLIGHT, METHOD FOR DETERMINATION OF MISSILE ATTITUDE AND DEVICES FOR THEIR REALIZATION | 2002 |
|
RU2218550C2 |
VARIABLE-STRUCTURE PNEUMATIC REGULATOR | 0 |
|
SU748345A1 |
METHOD OF IDENTIFICATION OF LINEAR DYNAMIC SYSTEM | 2018 |
|
RU2675281C1 |
Authors
Dates
2023-02-06—Published
2022-10-08—Filed