Installation of DynaFlight-AirAgII & DynaFlight-Forest

Transcription

1 DynaNav Systems Inc Airport Way Pitt Meadows. BC, Canada, VY B THIS MANUAL CONTAINS HELPFUL HINTS ON: Installation of DynaFlight-AirAgII & DynaFlight-Forest DynaFlight Airborne Aerial Application Guidance and Management system

2 Overview of System Mounting GPS Antenna Overview Placement FIGURE Telemetry and/or Differential Antenna (if option installed) Overview Placement Processor box Overview Placement Overview 5 Placement 5 Product features 6 Control Grip or Switches 7 Overview 7 Placement 7 FIGURE 8 Product features 8 Dual Relay box 9 Overview 9 Placement 9 Wiring Harness Diagrams 9 Overview 9 Supplied Parts List 9 Basic DynaFlight-AirAgII airborne system contains: 9 Specifications: 0 Appendix Follows: 0 DynaViz Display Wiring Control Switch and Spray Sensing Relay Box TopHat Switch Layout 5 Mounting Plate Assembly Drawings 6

3 DynaNav Installation Manual Overview of System The DynaFlight-AirAgII system is a GPS based electronic guidance and data management system specifically designed as a tool for the pilot to fly parallel swath guidance for the application of seeds, fertilizer and chemicals for farm and forestry applications. It also gives guidance to return back to the job to continue his application after refill. The system automatically senses spray on and spray off for recording and displaying the real time map of the application and displays this to the pilot in his heads up display. The system comes with a built in satellite differential. Mounting GPS Antenna Overview As the GPS antenna has two functions, one, to view the full constellation of orbiting satellites and two, to view the geo-stationary differential broadcast satellite positioned over the equator, the antenna should have as much visibility of the full sky as possible. Placement IMPORTANT!! Make sure that the GPS Antenna is bonded to the Airframe. The GPS antenna should be mounted on top of the aircraft/helicopter and should take into consideration the following. See figures, & : On helicopters, mount the antenna as far forward on the top as possible while keeping the antenna as flat to the horizon as possible. This is to keep it away from the rotor mast as much as possible as well as lead the pilot to the spot. The antenna should be mounted high enough to see as much of the sky above and around so as the fuselage does not block the signal and as far forward as possible. Mounting on the tail would be a last resort and should only be done if Laser Gyro option is installed in the DynaFlight. Keep as far away from transmitting antennas as possible (at least inches) If this is not possible, please contact DynaNav for recommendations.

4 Antenna Placed Between FIGURE Telemetry and/or Differential Antenna (if option installed) Overview As the Telemetry/Differential antenna has to view the ground based broadcast antenna, the antenna should be outside the aircraft and have visibility of this base antenna. Placement The ideal location for this antenna is on the bottom of the helicopter and as vertical as possible with the following considerations: Keep away from other communications antennas as far as possible. Do not mount immediately next to gear struts of hook assembly The shorter the coax the better the range.

5 Processor box Overview The DynaFlight-AirAgII processor box contains all the electronics of the system. It has a mounting plate that is bolted to the rubber shock mount on the bottom (see:- Mounting Plate in appendix). This plate only requires mounting screws to attach therefore the extra tabs for mounting can be removed if necessary. Placement The processor box can be mounted either horizontal or vertical using the Mounting Plate. The Processor box should be mounted for easy access to the PC Card.

6 Pilot Display Overview The pilot display is intended to be a heads-up type of display to be mounted in the field of view of the normal operation of the pilot. As such this DynaViz display has multiple functions including the following: Guidance display to guide pilot on his parallel swaths. Pilot display for selecting CUSTOMER, AREA/FIELD, and SWATH WIDTH. A moving map display to show last sprayed location. Rotating Map Navigation. Placement DISPLAY 5

7 The display should be mounted to best suit the requirements of both the pilot and the specific aircraft/helicopter. This should take into consideration the following: It should be in the direct view of the pilot, so as not to obstruct his view outside the aircraft. The sun shroud (used on the EL type display) should be positioned for full screen visibility for the pilot while occluding direct sunlight on the screen. As the bottom mount can be tilted from 0 to 5 degrees to adjust for individual pilot needs, be sure the bottom plate is mounted to allow for individual pilot needs (tall or short). The front of the screen should be oriented to front of helicopter/aircraft to give guidance information that relates to helicopter/aircraft flight direction. Product features The connector plug for the DynaViz display can be switched from side to side to meet installation requirements whether harness enters from either left or right side. As the display represents the ground view, the display should be mounted as horizontal as possible so as the pilot can see the complete screen. The EL display can be viewed a quite extreme angles and can use either the tunnel sun shroud or the angled sun shroud. The connector plug is a LEMO connector that is simply pushed on (align red dots first) and simply pulled off to remove. 6

8 Control Grip or Switches Overview The control grip contains three primary switches that control the entire system. On our supplied ErgoGrip, two of these switches are contained in the single 5 way Top Hat switch and the other on a push button switch. It is the intention of the system for the pilot to have access to these switches on his grip, cyclic or his collective or a combination of both. Other than these switches, the DynaFlight system is wired to the dual interface box to sense spray on/off or other actions. Placement If the grip, cyclic or collective have a spare Top Hat switch, it can be wired directly to the connector on the Dual Relay box along with two other push buttons for the accept and the window operation. This Dual Relay box should always be used as it contains the transient spike protection circuitry. If the ErgoGrip - Collective switch box is used, it should be attached to the collective such as to not interfere with the normal operation and so the top hat can be operated with the thumb. The supplied ErgoGrip is to replace the existing control grip on the flight control stick. 7

9 Product features Collective Switch FIGURE With the grip or collective switch box in the pilots hands, the pilot will be able to change job functions while observing the display to keep his field of view outside the helicopter/aircraft, not inside the cockpit. 8

10 Dual Relay box Overview The dual relay box has multiple functions to interface the aircraft and the pilot to the DynaNav system. These functions are as follows: NOTE: THIS BOX MUST BE INSTALLED IN ALL INSTALLATIONS TO PROTECT THE COMPUTER. To interface to sense the spray on/off of the aircraft system. To protect the DynaNav from the electrical spikes generated by the relay action To protect the DynaNav system from static discharge on the control switches. To interface multiple styles of control switch assemblies or to the ErgoGrip control grip. Placement The relay box is connected directly to the DynaFlight interface harness, From the relay box two harnesses are connected, the spray on/off sense lines and the control switch module. This does not need to be hard mounted, however for vibration isolation, it would be best to Velcro or dual lock it to any secure surface. Wiring The Dual Relay wiring harness has sets of wires; Spray and Spray. For most installations only Spray is connected to sense that the pilot is applying material. For Pressure switches on the Spray Boom, make sure the pressure is well within the range of the normal boom pressure for spraying. The Cessna P/N S- 00- Hobbs pressure switch can be adjusted to the right pressure. You can also use a Honeywell/Hobbs P/N which is the same. Wiring Harness Diagrams Overview The diagrams attached to appendix are for the interconnect wiring of the DynaNav system. All wires on the harnesses supplied (except the control grip/box) Supplied Parts List Basic DynaFlight-AirAgII airborne system contains: Part Number... Description ) DBII-586-GDEuroJavad.. DynaByte-AirAgII Processor/GPS Box ) DV-EL DynaViz Electro-luminescent display unit ) DV-Cable-0... DynaViz-Cable 0 foot Display cable pre-wired ) B06A-XT-... GPS, GLONASS, L Band Antenna 5) DB-AntCable... Antenna Cable ' TNC 6) DB-Cable.... DynaByte control cable ' DynaByte to Dual Relay foot 7) ErgoGrip / Switch kit... Military spec 5 way Top Hat control switch as well as other switches with 7 foot cable assembly. (for Helicopters, switches provided) 8) DB Dual relay box for dual sensing of spray on/off 9) DB-cable9... Spray on/off 9 ft. wire and plug 0) DB-PowerCable... MS Power Cable 8"with 5' ext. ) DynaByte-Mount Rack... Mounting Bracket plate assembly ) Ag Complete Key Card... Ag Complete Software and KEY CARD Compact Flash ) Dual Lock... feet peel and stick locking fastener ) Pelican Shipping Carrying Case 9

11 Specifications: Includes WAAS/EGNOS Real Time differential correction (RTCM 0 specification) to sub-meter accuracy. DynaNav basic ErgOS operating system with DynaFlight-AirAg version.0 software template. DynaViz Display Unit EL flat panel display showing position, moving-map, guidance and operating buttons, for a safe operation. DynaByte Rugged environmentally resistant enclosure with military spec. connectors, with Installation kit and cables Rugged ErgoGrip hand grip for fixed wing or Switch Kit for helicopters, for intuitive operator input Software file of Installation and Operations manual and quick reference user guide GPS Engine is sub-meter with less than 0. second latency and presented at sixteen position solutions per second or better. Specifications Environmental: Physical: DynaByte Processor DynaViz Display Unit Operating Temp: -0 to +50 degrees C. Width: 7.5 ins (8.5 cm) 6.5 ins (6 cm) Storage Temp: -0 to +70 degrees C. Height: 6.5 ins (6.5 cm) 5.5 ins ( cm) Humidity: 5 to 95%, non-condensing. Depth: 5 ins ( cm) 6.5 ins (6 cm) EMI/RFI: DOC, FCC Weight:.8 lbs (.7 kg).6 lbs (.6 kg) Installation kit including ErgoGrip and antenna weights are dependent on installation, typically less than lbs. (.kg) 8 0 VDC, negative ground (system requires less than watts) Note: Specifications subject to change without notice. Appendix Follows: 0

12 DynaViz Display Wiring

13 DB--- Dual Relay Box and Power Input Plug

14 I/O Control Box Wiring Diagram

15

16 TopHat Switch Layout 5

17 Mounting Plate Assembly Drawings 6

18 GPS ANTENNA VDC OUT REGULATED K VDC OUT REGULATED J 5 VDC OUT H GROUND G GROUND F POWER SEE NOTE SEE NOTE 0 E 0 D BUS C DYNAVIZ CABLE 5A 8-0 VDC IN B GROUND A MIL 0 CONNECTOR BASIC PP6 BUS AND MOD SEE NOTE 5 TELEMETRY LD LD0 LD LD 5 CP-CLK DYNAVIZ 7 H SYNC 9 Y SYNC 6 GROUND 0 +5 VDC 8 + VDC INTEGRATED FLIGHT GUIDANCE INSTRUMENT LEMO CONNECTOR GPS RG-58 DB-II-586 PROCESSOR LD DISPLAY Y LD0 Z LD AA LD BB CP-CLK GG H SYNC FF Y SYNC HH GROUND JJ +5 VDC N + VDC P CONTROL/COLLECTIVE STICK 5 WAY POSITION SWITCH DB-- DUAL RELAY BOX AMP CPC CONNECTOR MIL CONNECTOR BROWN MM RED BOTTOM BUTTON (TOP HAT) TOP BUTTON (TOP HAT) CONTROL AMP CPC CONNECTOR NN LEFT BUTTON (TOP HAT) TOP BUTTON (TOP HAT) LEFT BUTTON (TOP HAT) BOTTOM BUTTON (TOP HAT) RIGHT BUTTON (TOP HAT) QQ BLACK RIGHT BUTTON (TOP HAT) TT ORANGE ENTER BUTTON GG BLUE 7 SPRAY ON PP GREEN 6 SPRAY ON KK YELLOW 5 WINDOW BUTTON RR PURPLE 8 8 WINDOW BUTTON COMMON HH GREY & WHITE 9 9 COMMON SPARE LL CONTROL CABLE 7 SPRAY ENTER ENTER BUTTON 6 SPRAY 5 WINDOW 0 GPS IPPS (MARK INPUT) SS 0 GPS IPPS MARK INPUT C QTY. FUSE/CIRCUIT BREAKER MS SWITCH 0 WIRING DIAGRAM PART NO. ITEM DESCRIPTION LIST OF MATERIALS CONTROL GRIP SPRAY SPRAY AMP CPC CONNECTOR (AMP 065- MATING CONNECTOR) (AMP CLAMP) COMMON GND E +5 VOLTS U GPS COM RXD A GPS COM TXD W E COMMON GND PROCESSOR RXD TO EXT TXD S AIRCRAFT GROUND (A/C POWER IF DETECTION SWITCH IS GROUNDED) CONNECT TO AIRCRAFT SPRAY DETECTION SWITCH (NORMALLY OFF) OPTIONAL - CLOSING GATE DETECTION SWITCH (NORMALLY OFF) AIRCRAFT GROUND (A/C POWER IF DETECTION SWITCH IS GROUNDED) JJ WHITE/ORANGE X WHITE/BLUE U WHITE CONTROL/COLLECTIVE STICK 5 WAY POSITION SWITCH AUXILLIARY CONNECTIONS DB-II-586 PROCESSOR used with I/O Control Box Modified Harness for Mil AMP 55- CPC MINI CONNECTOR (AMP 550- CPC MATING CONNECTOR) (AMP 570- CLAMP) GPS COM DATA DB-ControlBox I/O CONTROL BOX PS CLK KEYBOARD 6 PS DATA KEYBOARD &5 5 Volts VCC TOP BUTTON (TOP HAT) LEFT BUTTON (TOP HAT) BOTTOM BUTTON (TOP HAT) RIGHT BUTTON (TOP HAT) 5 ENTER BUTTON 6 WINDOW BUTTON 9 COMMON 8 SPARE HH SHIELD 6&0 WHITE/BLUE SPRAY KK WHITE WHITE SPRAY QQ GREY SHIELD RELAY CONTROL LOGIC FF BLACK 7 RELAY CONTROL LOGIC EE BROWN 8 7 SPARE RELAY CONTROL LOGIC DD RED 0 SPARE WHITE/ORANGE COMMON PROCESSOR TXD TO EXT RXD R RELAY CONTROL LOGIC CC ORANGE SPARE COMMON GND M WHITE RELAY CONTROL LOGIC 5 BB YELLOW M SPARE SHIELD COMMON GND RELAY CONTROL LOGIC 6 AA GREEN SPARE RELAY CONTROL LOGIC 7 Z BLUE 9 SPARE Y VIOLET 5 PROCESSOR RXD TO EXT TXD B PROCESSOR TXD TO EXT RXD D E COMMON GND WHITE/BLUE FLOW CONTROL LASER DATA MIL CONNECTOR. IDENTIFY, ROUTE AND SECURE ALL WIRING AS PER AC.-A, CHAPTER, SECTIONS AND 7.. IF DESIGNATED FUSE/CIRCUIT BREAKER LOCATION IS USED BY OTHER INSTALLATION, LOCATE 5 AMP FUSE/CIRCUIT BREAKER IN CONVENIENT UNUSED LOCATION IN FUSE PANEL. LABEL FUSE "DYNANAV".. ALL WIRING UNLESS OTHERWISE MARKED IS MIL-W-759/6. THE LAST DASH NUMBER INDICATES WIRE GAUGE. 5. ATTACH GROUND TO EXISTING GROUND SCREW. RELAY CONTROL LOGIC 8 WHITE GPS IPPS (MARK INPUT) MM SHIELD GPS IPPS MARK INPUT C AMP 550- CPC MINI CONNECTOR (AMP 55- MATING CONNECTOR) (AMP 570- CLAMP) NOTES. LOCATE SWITCH ON PANEL CONVENIENT FOR PILOT AND LABEL "DYNANAV". WHITE/BLUE RELAY CONTROL OUT 0 5 RELAY CONTROL OUT 6 RELAY CONTROL OUT RELAY CONTROL OUT RELAY CONTROL OUT 5 0 RELAY CONTROL OUT 6 9 RELAY CONTROL OUT 7 LOW LEVEL OUT 0 LOW LEVEL OUT LOW LEVEL OUT 8 LOW LEVEL OUT LOW LEVEL OUT LOW LEVEL OUT 5 9 LOW LEVEL OUT 6 8 LOW LEVEL OUT 7 WINDOW To CONTROL GRIP RELAY CONTROL OUT ENTER SPRAY SPRAY AIRCRAFT GROUND (A/C POWER IF DETECTION SWITCH IS GROUNDED) CONNECT TO AIRCRAFT SPRAY DETECTION SWITCH (NORMALLY OFF) OPTIONAL - CLOSING GATE DETECTION SWITCH (NORMALLY OFF) AIRCRAFT GROUND (A/C POWER IF DETECTION SWITCH IS GROUNDED) AUXILLIARY CONNECTIONS Pitt Meadows BC Canada TITLE DynaFlight-AirAg Wiring Block Diagram DRAWING NO SCALE FILE NAME DATE Wiring Block Diagram AirAg : REVISION Feb SHEET of