super cyclops manual beta
Contents
1. AWB ZkLE RS Linear distance to the take off KALAM OLA Current azimuthal angle of the plane GPS 8 5 32 GPS signal intensity VAM ZS 2S FARE pitch attitude angle Asa WM ZSAS FA PE ik CASI JE Main board Video voltage 2H 71 HH Motor voltage zJ JJ Fy Motor current La Course SAR AHINLIEIZE Course difference against the destination HBE Ground velocity fai Altitude 22 Air velocity CYA FE 77 Consumption of motor power 5 H RAAHE Ground projector distance to the destination K4TY Ta Flying time At this time GPS starts searching the satellite signal The signal intensity symbol at the upper right corner refers to the number of the satellites detected If the signal intensity symbol flashes it means no satellite signal detected or the satellite signal date received by GPS is not reliable and cannot be used as location parameters The searching lasts one to five minutes in case of adequate satellite signal and the time changes in different environment Cautions 1 Please press RESET to Clear before taking off The operation will Clear altitude distance time and power consumption 2 The meaning of current azimuthal angle of the plane The location where there plane occupies is based on the take off as the base point and the rotates from due north from O to 360 degree For example if the plane is at the southeast direction the it will display 135 ZR east F south P west JE north LTH course KALLE plane location it2. SCR_In OSD display Receiver knob switch PWM switch channel Shift between manual control PA AUTOPILOT RTH Cautions 1 Never touch the pressure sensor with anything keep it clean and free from explosion to light 2 Never pressurize the air speed indicator in case damage may occur 3 Keep the circuit board away from electromagnetic field such as video projector and remote controller protector 4 Never touch the circuit board with metal in case short circuit may occur 5 Keep away from propeller movement range at least 1 5 times of the propeller diameter to the assistant in case deviations may occur to the air speed indicator 6 Please fit the infrared ray sensor to the plain as indicated in the following diagram DERS A IRSE HERAS E White arrow directing upward MEE RAKE EAZI Two sensors horizontally and vertically installed HERA AALS 77 A White arrow directing the plain head Description of display The main board indicator lamp flashes after power is connected The following picture will appear when you insert TF card Mini SD card If there is not TF card then it will display NO SD CARD FOUND and jump to startup picture automatically after 2 seconds CYCLOPS CYCLOPS FPU ASSISTANT HO SD CARD FOUND About 5 seconds later the system will enter pilot interface z wms SP BR 8 MEAS SBE SARAAN ER W BE y MIRE hjek m B16 B16 a i K4T ELLE Milelage H
3. infrared ray attitude sensor is newly fitted 3 If there is TF card mini SD card and power supply is connected TF card will generate USERID txt file in which 30 digit ID number of the main board will be stored Please keep the number properly for future maintenance and software updating Description of auto pilot 1 Please confirm that infrared ray sensor and airspeed pipe are properly installed and the infrared ray attitude sensor shall not bear large angle deviations from the plane 2 We recommend the clients to use model plane with good stability 3 Flying mode shift shall be connected to any knob ratio channel on the remote controller Under different modes the flying interface will display different information PA auxiliary manual pilot mode AUTOPILOT auto pilot mode RTH Auto return mode At auto pilot mode turn the knob AUTOPILOT to PA and quickly back to AUTOPILOT the system will shift to the next waypoint iyo oF ah a i PARER wai ia En wM ja Faa auxiliary manual pilot mode H3 auto pilot mode 43 manual pilot mode H JRNL auto return mode 4 We recommend to use remote controller with failure protection functions F S function You may set plain pilot mode shift channel failure protection as auto return pilot In this case the plane can automatically return in case of failure 5 In PA mode the system can keep the course and altitude automatically and the screen will display to LOCK symbols as fo
4. CYCLOPS FPV ASSISTANT V1 0 User s Manual Beta Version The product is an assistant flying equipment with OSD auto pilot functions for FPV fans The product has the advantages of small size light weight well developed functions and simplified operations Hardware configurations Description of the cables Jumper number ae utront sensor interface TF card socket See Table 1 l gt Horizontal IR sensor interface Vertical IR sensor interlace ita CYCLOPS Switch toara inertas f di FPV ASSISTANT gba DES odin iias K es z _ T plug should be purchased alone Table 1 PCB Functions Equipment connected Signal mode Remarks indications battery battery JP Jumper If only the power is 12V or 3S Lipo battery the main board can use the power 1 and 2 short circuit for power supply of main board 2 and 3 short circuit for power supply of battery power and the main board NTSC PAL Automatic detection of video signal power supply consistent with the V_OUT Video frequency main board voltage V_IN Video input NTSC PAL Automatic detection of video signal power supply consistent with the main board voltage output AIL _OUT Aileron PWM steering engine output ELE_Out Elevator Elevator steering engine PWM steering engine output output steering engine AIL In PWM ELE_In PWM THO_In PWM AUX_In PWM MOD _In Pilot mode Receiver knob channel PWM shift
5. KA take off 3 Position indication in return travel H in the screen refers to the take off A G refer to destinations when the take off point is in front of the plane then it displays H when the take off point is at the back of the plane H will flash If H is in the middle and does not flash it means that the plane is travelling back to the take off point If H is in the middle and flashes it means that the plane is deviating from the take off point at 180 degree Methods for return travel H is displayed at the left side turn left to travel back If H is displayed at the right side turn right to travel back Description of menu parameters setting Press UP and DOWN to enter main menu setting interface MENU SYSTEM CONFIG WAYPOINT EXIT SYSTEM CONFIGU SETTING DESCRIPTION Page 1 ATT DATA If the attitude angle parameters If the environment is not suitable for flying the displayed in the flying interface attitude angle parameters in flying interface will flash BAT SCALE Battery scale setting If the power consumption reaches the value set during the flying the battery scale symbol will flash RESET Clear current sensor Clear the first application or after current sensor RESET Clear air speed Re clear the air speed if the environment SERVO Confirm the servo center You need to confirm the servo center after you CENTER change the model aeroplane Please manually fly the plane and adjust the servo center Reversal
6. hen update progression is 100 the screen will display as follows for system checking CYCLOPS UPDATING 100Z CHECKING After the checking the screen will display as follows CYCLOPS UPDATING 100Z SUCCEEDED At this point you finishes update After update the system will automatically run the new program If the update fails the screen will display as follows CYCLOPS UPDATING 1 B0B0Z ee The following cases may result in update failure 1 Update program is not available in TF card 2 Update program is corrupted 3 Update program does not match product ID
7. llows If the operator control aileron direction steer or elevator steer the course or the altitude lock will be released At this time the system will automatically control the plane attitude according to the control amount of the operators For example if the aileron is in 100 amount the plane will fly left right at 45 degree slope if the elevator steer is in 100 amount the plane will lift lower at 20 degree angle Until the control lever returns to the neutral the system will lock and keep the course and altitude at the moment Additional functions When TF card is inserted into the system and the system detects satellite signal press for seconds UP button and SD symbols will appear on the upper right corner and flash At this point the card starts storing the system data Press Reset and the card will restart storing the system data If you want to end data storage press UP button for 3 seconds and SD card symbol stops flashing and you end data storage Description of software updating CYCLOPS FPV ASSISTANT may be updated with TF mini SD card We will issue the update programs on Internet The clients may download the update program and copy it to the TF card 1 Download Update cyc 2 Copy Update cyc to TF card and insert TF card into CYCLOPS FPV ASSISTANT main board 3 Press OK and start up the system release the button when you see the following picture until the update is finished CYCLOPS UPDATING W
8. point The operators need to turn the knob manually to shift to the next waypoint T MAXISCHG Advance distance for Setting range 0 100 meters waypoint shift NOTE The system is in default value at leaving factory The clients need only to set the red bold characters for auto pilot Operations 1 REV reversal setting Cover the upper part Z axis infrared ray of the vertical infrared ray sensor Z axis infrared ray with a hand after proper connections confirmed shift the flying mode to PA mode Then cover the left side and front of the horizontal infrared ray sensor XY axis infrared ray observe whether the aileron is calibrated to the right side and the elevator steering engine is properly adjusted If not adjust AIL and ELE of REV options If motor is used as the model plane throttle channel the reversal 1s available for default value The clients only need to the remote controller throttle channel 2 TRIM infrared ray sensor trim setting After infrared ray sensor is fitted on the model plane put the plane higher than the head in the open space and observe the attitude angle parameters if P parameters is negative number such as 3 you need to adjust P parameters to 3 Repeat the operations and observe P parameters until it becomes 0 Observe R parameters with the methods as mentioned above to trim R parameters You need only conduct the operations once after the infrared ray sensor is properly fitted unless the plane is changed or
9. setting Refer to Operation instruction 1 TRIM Trim the infrared ray sensor Refer to Operation instruction 2 Page 2 CRUISE Set cruise airspeed Airspeed value 0 200Km h during auto pilot AIRSPEED when set as 0 the system will not control the airspeed SPEEDMAX_ Maximal limit of airspeed The air speed of the throttle in PA mode LIM SPEEDLOW _ Lowest limit of airspeed When the air speed of the model plane is lower LIM than the value set the system will not f u ascent to avoid speed loss ELEVON Used to control aileron type model plane If choose Y close compound control setting on the remote controller projector ROLL Roll control parameters SEV k ANG maximal slope limit at turn PITCH Pitch control parameters SEV f st ANG maximal angle limitat pitch Description of waypoints Page 1 page 2 DIS Waypoint distance The distance between the Waypoint and the home point setting range 0 5000meters ANGLE Waypoint angle The angle between the line of waypoint and the home point with the due north setting range 0 359 Altitude of waypoint Setting range 0 800 meters RAD Hovering radius The hovering radius with the waypoint as the center setting range 0 500 meters DR oO Hovering direction L counterclockwise R clockwise ON OFF Whether to use the er Page 3 AUTOWAYPOIN Auto waypoint shift Y Shift to the next waypoint after the plane reaches the waypoint N hover as set above the current way
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