FIELD: aviation.
SUBSTANCE: to implement the maneuver, the initial boundary guidance problem is divided into a set of intermediate boundary problems, in which the required values of the control parameters for the aerodynamic bank and the angle of attack, calculated for each reference point in each guidance cycle, are small throughout the guidance time, and stick force on the aerodynamic controls of an unmanned aerial vehicle is formed.
EFFECT: reducing of speed and time of motion loss of unmanned aerial vehicle.
3 dwg, 2 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF CONTROLLING UNMANNED PLANNING AERIAL VEHICLE | 2017 |
|
RU2654238C1 |
| CONTROL METHOD OF AN UNMANNED GLIDING AIRCRAFT ON TRAJECTORIES WITH CHANGES OF DIRECTIONS OF MOVEMENT IN THE SPECIFIED REFERENCE POINTS | 2019 |
|
RU2708412C1 |
| METHOD FOR FORMATION OF MANOEUVRES OF ARBITRARY CONFIGURATION ON TERMINAL TRAJECTORY OF UNMANNED GLIDING AERIAL VEHICLE | 2013 |
|
RU2554568C2 |
| METHOD OF LANDING UNMANNED AERODYNAMIC FLYING VEHICLE | 2005 |
|
RU2278801C1 |
| METHOD OF CONTROLLING TOWING SYSTEM (TOW AIRCRAFT -TOWING CABLE - TOWED AIRCRAFT) | 2007 |
|
RU2347719C1 |
| METHOD FOR CONTROLLING SPACECRAFT MOTION ON ACTIVE SECTION OF PLACING IT INTO THE ORBIT OF PLANET ARTIFICIAL SATELLITE | 2015 |
|
RU2596004C2 |
| METHOD FOR INCLUDING PREFORMED MANEUVER IN FLIGHT TASK OF UNMANNED GLIDING AIRCRAFT | 2020 |
|
RU2756964C1 |
| SPACE VEHICLE FOR DESCENT IN ATMOSPHERE OF PLANET AND METHOD OF DESCENT OF SPACE VEHICLE IN ATMOSPHERE OF PLANET | 1994 |
|
RU2083448C1 |
| METHOD FOR DETERMINING AIRCRAFT AERODYNAMIC CHARACTERISTICS BASED ON FLIGHT EXPERIMENT RESULTS | 2022 |
|
RU2790358C1 |
| METHOD OF GUIDANCE OF UNMANNED FLYING VEHICLE IN GLIDE CONDITIONS | 2004 |
|
RU2286590C2 |
