uAvionix Ping200S Скачать руководство пользователя страница 12 | Manualshive

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UAV-1000711-001

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12 | 34

6 Technical Specifications

Specification

Characteristics

Compliance

TSO-C199 Class A
Level 2e Class 1 DO-181E
Class B1S DO-260B

FCC ID

2AFFTP200S

FAA Transmit
License

Manned aircraft. Un-manned operating above 500ft
AGL.

Software

RTCA DO-178B Level C

Hardware

RTCA DO-254 Level C

Power
Requirements

11

– 33VDC. Typical 2W.

Altitude

35,000ft

Operating
Temperature

-45°C to +70°C

Humidity

Tested to Category DO-160G Category B2

Transmit
Frequency

1090MHz ±1MHz

Transmit Power

250W nominal; 125W minimum at antenna after
allowing for 0.5dB connector losses and 1.5dB cable
losses.

Transmitter
Modulation

6M75 V1D

Receiver
Frequency

1030MHz

Receiver
Sensitivity

-74dBm ±3dB

Weight

50grams

Height

17mm

Length

59mm

Width

57mm

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Содержание Ping200S

Страница 1: ...UAV 1000711 001 Page 1 34 Ping200S User and Installation Guide ...

Страница 2: ...y storage medium for any purpose without the express written permission of uAvionix uAvionix grants permissions to download a single copy of this guide onto an electronic storage medium to be viewed for personal use provided that the complete text of this copyright notice is retained Unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited uAvionix is a reg...

Страница 3: ...UAV 1000711 001 Page 3 34 1 Revision History Revision Date Comments A 10 21 16 Initial release ...

Страница 4: ... not liable for damages arising from the use or misuse of this product This equipment has received a FAA transmit license for manned aircraft and a license for un manned aircraft operating above 500ft AGL This antenna used for this transmitter must installed to provide a separation distance of at least 20cm from all persons ...

Страница 5: ...sible for any transportation cost This warranty does not apply to cosmetic damage consumable parts damage caused by accident abuse misuse water fire or flood damage caused by unauthorized servicing or product that has been modified or altered IN NO EVENT SHALL UAVIONIX BE LIABLE FOR ANY INCIDENTAL SPECIAL INDIRECT OR CONSEQUENTIAL DAMAGES WHETHER RESULTING FROM THE USE MISUSE OR INABILITY TO USE T...

Страница 6: ... Markings 13 7 Equipment Limitations 13 7 1 Installation 13 7 1 1 Modifications and Use Outside of Intended Scope 13 7 1 2 Deviations 13 7 1 3 Configurable Options 13 7 1 4 Approvals 13 7 1 5 FAA Transmitter License and FCC Grant of Equipment Authorization 14 8 Equipment Installation 15 8 1 Unpacking and Inspecting 15 8 2 Mounting 15 8 3 Connections 16 8 4 Wiring Diagram 17 8 5 Cooling Requirement...

Страница 7: ...O Number 24 9 2 VFR Squawk Code 24 9 3 Callsign 24 9 4 Aircraft Maximum Speed 25 9 5 Aircraft Category 25 9 6 Aircraft VSO 25 9 7 Aircraft Size 25 9 8 GPS Antenna Offset 25 9 9 ADS B Rx Capability 26 9 10 Programming 27 10 Post Installation Checks 28 11 Continued Airworthiness 28 12 Environmental Qualification Forms 29 ...

Страница 8: ...ision avoidance systems In all cases the interrogations are received by the transponder on 1030MHz and replies are transmitted on 1090MHz This system will enable the aircraft to be visible to ATC and other aircraft equipped with Traffic Advisory System TAS as defined in TSO C174 Traffic Alert and Collision Avoidance System I TCAS I as defined in TSO C188 Traffic Alert and Collision Avoidance Syste...

Страница 9: ...e GDL 90 Compatible Control Protocol See Appendix A COM1 TX 57600bps Heartbeat Ownship Geometric Altitude GDL 90 See Appendix B COM2 RX 115200bps Reserved for future use Mutual Suppression Input Commonly used between transponders and DME systems and between transponders and collision avoidance systems FYXnav Interface Interface Specification Protocol FYXnav 115200bps GPS Altitude Encoder ICAO numb...

Страница 10: ... systems to track and display the TABS aircraft TABS are intended to be used on aircraft that are exempt from carrying a transponder or ADS B equipment such as gliders balloons and aircraft without electrical systems A TABS will allow these exempted aircraft to be visible to other aircraft equipped with Traffic Advisory System TAS as defined in TSO C147 Traffic Alert and Collision Avoidance System...

Страница 11: ...ber Revision Ping200S UAV 1000706 001 A Power Adapter UAV 1000707 001 A Ping200S Power Adapter Cable Power Adapter Battery Cable A FYXnav TSO GPS Baro UAV 1000568 001 A Ping200S FYXnav Cable UAV 1000595 001 A PingBuddy UAV 1000525 001 A Programmer USB Micro Cable Dipole Antenna UAV 1000653 001 A 4S 800mAHr LiPo Battery AC Charger Fastener Set FYXnav Mounting Tape Ping200S User Manual UAV 1000711 0...

Страница 12: ...B Level C Hardware RTCA DO 254 Level C Power Requirements 11 33VDC Typical 2W Altitude 35 000ft Operating Temperature 45 C to 70 C Humidity Tested to Category DO 160G Category B2 Transmit Frequency 1090MHz 1MHz Transmit Power 250W nominal 125W minimum at antenna after allowing for 0 5dB connector losses and 1 5dB cable losses Transmitter Modulation 6M75 V1D Receiver Frequency 1030MHz Receiver Sens...

Страница 13: ...evice with any antenna other than the one shipped with the device 7 1 2 Deviations There are no deviations from the MPS of TSO C199 Class A Device 7 1 3 Configurable Options Accessing or altering configurable options not intended to be operated may cause pilot distraction 7 1 4 Approvals Approvals do not cover adaptations to the aircraft necessary to accommodate ancillary equipment such as power p...

Страница 14: ...d in 14 CFR 91 225 7 1 5 FAA Transmitter License and FCC Grant of Equipment Authorization This equipment has received a FAA transmit license for manned aircraft and for un manned aircraft operating above 500ft AGL This equipment has been issued an FCC Grant of Equipment Authorization The equipment contains FCC ID 2AFFTP200S and is marked on the equipment nameplate ...

Страница 15: ...d all packing materials 8 2 Mounting The Ping200S is designed to be mounted in any convenient location in the cockpit the cabin or an avionics bay The following installation procedure should be followed remembering to allow adequate space for installation of cables and connectors Select a position in the aircraft that is not too close to any high external heat source The Ping200S is not a signific...

Страница 16: ...000711 001 Page 16 34 8 3 Connections Whenever power is supplied to the transponder a 50ohm load must be provided to the SMA connection You can use the supplied antenna or a commercially available 50ohm load ...

Страница 17: ...11 001 Page 17 34 The following diagrams illustrate the setups using 48V and 14 28V Aircraft power Note that a power adapter will be required when installing with 14 28V Aircraft power 48V 46 52V Aircraft Power ...

Страница 18: ... COM2 RX RS 232 In 115200bps RFU 6 SURPRESS 3 3V IO Mating Connector Molex 0436450600 Pins 0462350001 FYXnav Interface Pin Type Physical Rate Link 1 RX In 3 3V Serial 115200bps uAvionix 2 TX Out 3 3V Serial 115200bps GDL 90 3 Power 5V Out 4 Ground Mating Connector JST ZHR 4 Pins SZH 002T P0 5 LEDs LED SOLID FLASHING RED FAULT Reply Transmit GREEN Powered Receiving Interrogation ...

Страница 19: ...cent audio wiring if it is not possible to route them separately The distance between the Ping200S and the power adapter is limited by the impedance of the wire between them The Ping200S is powered from the power adapter not directly from aircraft power and therefore the acceptable voltage drop in the power line is what limits the distance The Ping200S needs an impedance of less than 0 5ohm in the...

Страница 20: ...om landing gear doors access doors or other openings which will break the ground plane for the antenna The antenna should be mounted in a vertical position when the aircraft is in level flight Avoid mounting the antenna within 1 meter of the ADF sense antenna or any COMM antenna and 2 meters from the transponder to the DME antenna Where practical plan the antenna location to keep the cable lengths...

Страница 21: ...onventional aircraft monopole antenna is used it relies on a ground plane for correct behavior For ideal performance the ground plane should be large relative to the wavelength of the transmission which is 275mm In a metal skinned aircraft this is usually easily accomplish but is more difficult in a composite or fabric skinned aircraft In these cases a metallic ground plane should be fabricated an...

Страница 22: ...s or has foil and braid screen Once the cable run length is known a cable type with low enough loss per meter that meets the above requirements can be chosen Longer runs require lower loss cable The following table is a guide to the maximum usable lengths of some common cable types Actual cable loss varies between manufacturers There are many variants and the table is based on typical data Use it ...

Страница 23: ...es such as ignition wiring 400Hz generators fluorescent lighting and electric motors Allow a minimum separation of 300mm from an ADF antenna cable Keep the cable run as short as possible Avoid routing the cable around tight bends Avoid kinking the cable even temporarily during installation Secure the cable so that it cannot interfere with other systems ...

Страница 24: ...DS B RX Capability UAT RX NO ES1090 RX NO Configuration Items List 9 1 ICAO Number The ICAO address is a 24 bit number issued to the aircraft by the registration authority of the aircraft These addresses are usually written as a 6 digit hexadecimal number although you may also encounter one written as an 8 digit octal number The FYXnav understands the hexadecimal format An octal number must be con...

Страница 25: ... conflicts Enter the length and width wingspan fields and the appropriate size codes will be calculated for transmission 9 8 GPS Antenna Offset The GPS antenna offset is used in conjunction with the length and width to manage taxiway conflicts A typical GPS does not report the geographic position of the center of the aircraft or even the tip of the nose of the aircraft instead it usually reports t...

Страница 26: ...V 1000711 001 Page 26 34 9 9 ADS B RX Capability The ADS B transmissions include an indication to the ground stations of whether the aircraft includes a 1090MHz ADS B receiver a UAT ADS B receiver or both ...

Страница 27: ...upplied Wi Fi adapter and mobile device application Please refer to the following documentation FYXnav datasheet http uavionix com downloads pingnav docs uAvionix PingNav Data Sheet AP4 pdf FYXnav quick start guide http uavionix com downloads pingnav docs uAvionix Ping Nav Quick Start Guide pdf Ping App iOS quick start guide http uavionix com downloads pingapp uAvionix ping app Quick Start Guide p...

Страница 28: ...uirement is also generally due to antenna or wiring issues Verification of the GPS position source and ADS B outputs Whenever a valid position is received by the transponder and the transponder is in any mode other than standby ADS B Extended Squitter messages should be observed on the transponder test set 11 Continued Airworthiness Other than for periodic functional checks required by the regulat...

Страница 29: ...ype 5 Vibration 8 0 Aircraft zone 2 type 3 4 5 to Category S level M type 1 Helicopters to Category U level G Explosion 9 0 Equipment identified as Category X no test Waterproofness 10 0 Equipment identified as Category X no test Fluids Susceptibility 11 0 Equipment identified as Category X no test Sand and Dust 12 0 Equipment identified as Category X no test Fungus 13 0 Equipment identified as Ca...

Страница 30: ...ited with a carriage return character A1 Physical Interface The Control interface uses RS 232 signaling levels The port is configured for the following characteristics Baud Rate 57600 baud Start Bits 1 Data Length 8 Stop Bits 1 Parity None Flow Control None A2 Control Messages The following table summarizes the Control messages that the Ping200S receives Msg ID Description Notes Ref CS Call Sign 1...

Страница 31: ...ble call sign Byte Contents Description 1 ASCII 0x5E 2 C ASCII C 0x43 3 S ASCII S 0x53 4 ASCII space 0x20 5 12 dddddddd ASCII call sign all 8 characters are mandatory right pad with space 13 14 dd Checksum of bytes 1 through 12 In hex ASCII i e FA 15 r ASCII carriage return 0x0D Example CS UAVIONIX87 ...

Страница 32: ...ergency field table below 14 h Health bit in hex ASCII 1 15 16 dd Checksum of bytes 1 through 14 In hex ASCII i e FA 17 r ASCII carriage return 0x0D Mode Field m Definition ASCII O Standby Mode 0x4F A Mode A 0x41 C Mode C 0x43 S Mode S 0x53 Ident Field i Definition ASCII I Ident Enabled 0x49 Ident is Inactive 0x2D Emergency Field e Definition ASCII 0 None 0x00 1 General 0x01 2 Medical 0x02 3 Fuel ...

Страница 33: ...that is used to indicate the VFR operating condition Byte Contents Description 1 ASCII 0x5E 2 V ASCII V 0x56 3 C ASCII C 0x43 4 ASCII space 0x20 5 8 dddd ASCII VFR code ASCII characters 9 10 dd Checksum of bytes 1 through 10 In hex ASCII i e FA 11 r ASCII carriage return 0x0D Example VC 1200DA VFR code is 1200 ...

Страница 34: ...nterface Specification can be found at https www faa gov nextgen programs adsb wsa media GDL90_Public_ICD_RevA PDF Ping200S transmits the following messages Msg ID Description Notes Ref 010 Heartbeat 1 second interval 3 1 1010 Ownship Report 1 second interval 3 4 1110 Ownship Geometric Report 1 second interval 3 8 ...

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