SP120C Autopilot User Manual (V3)

Total Page:16

File Type:pdf, Size:1020Kb

SP120C Autopilot User Manual (V3) SP120C Autopilot User Manual (v3) SI-TEX Main Office Address: 25 Enterprise Zone Drive, Ste 2 Riverhead, NY 11901 Tel: +1-631-996-2690 Email: [email protected] Web: www.si-tex.com IMPORTANT: PLEASE RETAIN ON BOARD (This page intentionally left blank) Contents Warnings 2 Important Installation Notes 3 Installation Tools Required 3 Overview 4 Standard Equipment 4 Additional Equipment Required 4 System Block Diagram 5 System Components / Installation Guides 5 SP120C Control Display Unit 5 Installation Dimensions and Guide 6 Electronic Compass 6-7 Rudder Feedback Unit 8-10 Installation and Wiring 11-13 System Operation 13-14 Steering Modes 13-14 Display Screens 15 System Settings 16 Pilot Settings 16-19 Advanced Menus 20-21 Initial Setup (Installers Instructions) 22 Calibration 22 GPS Settings 25 Other Menu Items 26 Setting Up And Configuring Your GPS System 26 Initial Inspection And Testing 28 Dockside Tests 28 Error Messages 29 Alarms 29 Trouble Shooting 30-31 Warranty 32 Additional Information 33 Contact Information 34 Warnings • The autopilot is a navigational aid; an adequate watch must be maintained at all times when autopilot is in use. • The autopilot must be placed in manual mode when the vessel is stationary as the system may continue to drive the rudder to the end of its travel and damage to the system may result. • It is strongly recommended that the autopilot not be used while navigating in restricted waterways as water currents, wind changes or radio transmitter interference can endanger your own or other vessels. • It is recommended to install a rudder feedback unit for best performance; otherwise the system will not operate in auto / gps mode unless the vessel is moving at a configurable minimum speed. 2 of 34 SI-TEX Marine Electronics - SP120C Color Autopilot Important Installation Installation Tools Notes Required • Access for wiring must be provided. • Screwdrivers – flat blade and cables will possibly need to be phillips head run or extended if required, to the • Side cutting pliers vessels switchboard, SP120C display, e-compass, rudder • Wire strippers feedback (if fitted) and drive unit. • Spanners (various) or adjustable • SP120C cables and equipment spanner must be located as far as possible • 75mm hole saw from transmitting equipment and cables (e.g. radio aerials and • Power drill + assortment of drill bits aerial cables, radars, inverters, • Multi meter (dvm) ect) to prevent electro-magnetic- interference. • Ancillaries such as tape, terminal block, screws, cable ties, etc. • The e-compass must be mounted a minimum distance of 1 meter from other magnetic compasses, radios, speakers, transmitting equipment or other products with magnetic properties, to avoid interference. • The SP120C must have a direct connection to power supply via a 15 amp circuit breaker or a 15 amp fused circuit and an isolating switch. SI-TEX Marine Electronics - SP120C Color Autopilot 3 of 34 Overview System Block Diagram Standard Equipment • SP120C CDU ‘Control Display Unit’ • ELECOM - electronic compass / e-compass • RFUS - rudder feedback unit PILOT CONTROL (optional) DISPLAY UNIT Additional Equipment Required (not standard supply) 30CM FLYLEAD FOR BATTERY & MOTOR 1. Drive motor – to allow the CONNECTIONS SP120C to control the vessels CUSTOMER steering system. SUPPLIED • Hydraulic steering systems with CABLES & TERMINALS a helm pump and ram will require one of the following; • Reversing hydraulic motor/ pump-set, tapped into the 12 OR 24 VDC existing hydraulic steering BATTERY system or; *CUSTOMER SUPPLIED • A constant running hydraulic pump with direction control solenoids. A mechanical steering system will require; AUTOPILOT DRIVE UNIT • a reversing mechanical drive, RUDDER *CUSTOMER connected to the existing FEEDBACK SUPPLIED UNIT steering ram mechanism. *OPTIONAL 2. Termination hardware; • Terminal blocks (suitable for 0.75mm2 and 2.5mm2 cables) 10m SUPPLIED CABLE OPTIONAL • Circuit breaker / switch (15A GPS (NMEA I/F) *CUSTOMER rated) SUPPLIED • Wiring extension cables / ferrules / crimp lugs & related crimp tools 5m SUPPLIED CABLE • 2c x 2.5mm2 for extending motor and power cables (larger for long cable runs) 2 • 1 pair 0.75mm for each nmea ELECTRONIC interface cable COMPASS 4 of 34 SI-TEX Marine Electronics - SP120C Color Autopilot System Components / Installation Guides SP120C - Control Display Unit • Steering control system for 4.0m - 16m vessels; • ‘Virtual Rudder Feedback’ feature, where no RFU requires to be installed. • 3 Control Modes – Manual Mode, Auto Mode and GPS mode • Live indication for ‘Steering mode’, ‘Position & Waypoint Info’, ‘Heading’, ‘Course to Steer’, ‘Rudder angle’, • Additional auto switching fail ‘System Voltage’ and ‘Drive Current’ safes, in case of failure of RFU or • Supports all current NMEA-0183 E-compass; interface standards; • If RFU fails, the system will • Heading: HDG, HDT, THS, HDM/ revert to Non-RFU mode ROT & COG automatically. • GPS: APA, APB, XTE, BOD, BWC & RTR *for GPS steering mode • If a GPS system is connected and the standard supplied • GLL, RMC, SOG, VTG *for visual E-Compass fails, the SP120C indication and assisting AUTOPILOT system will automatically revert control to GPS ‘COG’ mode for heading • 30cm fly-lead for drive motor and reference. power connections • 6 pin LTW connectors for Compass and Rudder/NMEA-0183 interfaces • Power: 12-24 Volts DC (Up to 29V During Charging) • Drive output up to 35A. *If current exceeds 35A, the drive output is inhibited. • Software controlled rudder limits, inhibits drive control at each mechanical limit. SI-TEX Marine Electronics - SP120C Color Autopilot 5 of 34 Installation SP120C CDU Installation Dimensions 110mm 43mm Mounting holes are at 94mm square 110mm ELECOM SP120C CDU Installation Guide Electronic Compass - The SP120C Head unit should be (E-Compass V.3) mounted in a position accessible to Take care when handling the the steering position and protected compass as it is a sensitive piece of from direct rain or salt water. equipment. - For in dash mounting cut a 75mm The compass position is the most (3.0”) hole important item in the installation of - An optional mounting bracket the autopilot. Good course holding is available and may be used is dependent on the compass being for desktop mounting - see your free from magnetic interference and supplier excessive rolling or pitching. - Drill mounting screw holes E-Compass Specifications: - Mount the display using screws • Output based on NMEA 0183 supplied (304 SS – 6G) standards NOTE: Use the protection cover • Protocol Settings: 4800–8–N–1 when the system is not in use, to protect the screen and casing from • Output Sentences: HDM & ROT UV and other physical damage • Power supply: 12-24 VDC <1Watt • No moving parts to prevent mechanical wear-out, small size and high reliability. 6 of 34 SI-TEX Marine Electronics - SP120C Color Autopilot • Solid state electronics with tilt and • Check other side of bulkheads and roll compensation up to 35degrees. deck heads for magnetic interfering type objects before mounting. E-Compass Installation Guide: • Mount the compass horizontally • IMPORTANT! The compass must with the arrow (bow) pointing to the be fitted in an area at least 1 meter front of the vessel, preferably on a away from steel objects. stainless steel, wooden or plastic • Avoid positions near radios, bracket. speakers, aerials, antenna cables or • Use non-magnetic screws to mount any other current carrying cables. the compass unit (316 grade • Select a dry position free from stainless steel) magnetic interference. • The unit must be mounted on a flat • If system is fitted to a steel hull horizontal surface. vessel, the compass must be • Before selecting the E-compass mounted at least 1m above the steel installation position, it is good to structure on a non-magnetic post or test the installation position is free bracket (aluminium and wood are from interference by checking the good options in this case) location with a portable magnetic • A lower / aft mounted position along compass. the centre of the hull is preferred, to reduce the influence of vessel roll and pitch. E-Compass Dimensions SI-TEX Marine Electronics - SP120C Color Autopilot 7 of 34 Rudder Feedback Unit Rudder Feedback Unit (RFUS) RFU Installation Guide The RFU is optional, although 1. Refer to installation diagram and recommended for the best possible installation template supplied with performance on some types of the unit vessels. 2. Mount rudder feedback adjacent to For example: A RFU must be the tiller ( : rudder feedback installed on vessels with high sides NOTE movement must copy the angular that are sensitive to winds turning the movement of the tiller like a boat, or high powered 5-6m Deep V pendulum) (22-25 deg dead rise / 175HP+) type vessels used in rough seas and high 3. Use a mounting bracket if required. winds. Or any other vessels that are 4. Note the markings on the rudder overly sensitive and very responsive feedback unit. ‘P & S’ (Port and to small amounts of ‘rudder’ at high Starboard) to check ruder moves speeds. in the correct direction, manually, When the RFU is installed, the TO TO CONNECT 5 before testing on the water.RFU-S TMQ configuration RED settings 5V areRFU simplified. AP47C AP47C 0 6 RUDDER Non-RFU mode is slightly more 5. Check installation is suitable RUDDER RUDDER 0 GRN WIPER RFU Cable Supplied 14m FEEDBACK LTW-6PIN LTW-6PIN 0 complicated. by slowly moving the steering UNIT 4 4 manually, to ensure: NOTE: BLU The RFUS av is factoryRFU aligned. The arm should not be removed or a. The direction indicated on the loosened. It is also water resistant, top of the RFU is correct however, if mounted in a wet position b. No undue mechanical strain some protection should be provided is placed on the feedback to prevent water damage or physical or linkage. (Also check for damage. strain when the tiller is tilted upright (for outboard engine installations) 6. To complete the install, use the SP120C advanced menu to calibrate the rudder limits and centre point of the RFU.
Recommended publications
  • Acnmanual.Pdf
    Advanced Coastal Navigation Coast Guard Auxiliary Association Inc. Washington, D. C. First Edition..........................................................................1987 Second Edition .....................................................................1990 Third Edition ........................................................................1999 Fourth Edition.......................................................................2002 ii iii iv v vi Advanced Coastal Navigation TABLE OF CONTENTS Introduction...................................................................................................ix Chapter 1 INTRODUCTION TO COASTAL NAVIGATION . .1-1 Chapter 2 THE MARINE MAGNETIC COMPASS . .2-1 Chapter 3 THE NAUTICAL CHART . .3-1 Chapter 4 THE NAVIGATOR’S TOOLS & INSTRUMENTS . .4-1 Chapter 5 DEAD RECKONING . .5-1 Chapter 6 PILOTING . .6-1 Chapter 7 CURRENT SAILING . .7-1 Chapter 8 TIDES AND TIDAL CURRENTS . .8-1 Chapter 9 RADIONAVIGATION . .9-1 Chapter 10 NAVIGATION REFERENCE PUBLICATIONS . .10-1 Chapter 11 FUEL AND VOYAGE PLANNING . .11-1 Chapter 12 REFLECTIONS . .12-1 Appendix A GLOSSARY . .A-1 INDEX . .Index-1 vii Advanced Coastal Navigation viii intRodUction WELCOME ABOARD! Welcome to the exciting world of completed the course. But it does marine navigation! This is the fourth require a professional atti tude, care- edition of the text Advanced Coastal ful attention to classroom presenta- Navigation (ACN), designed to be tions, and diligence in working out used in con cert with the 1210-Tr sample problems. chart in the Public Education (PE) The ACN course has been course of the same name taught by designed to utilize the 1210-Tr nau - the United States Coast Guard tical chart. It is suggested that this Auxiliary (USCGAUX). Portions of chart be readily at hand so that you this text are also used for the Basic can follow along as you read the Coastal Navigation (BCN) PE text. We recognize that students course.
    [Show full text]
  • FAA-H-8083-15, Instrument Flying Handbook -- 1 of 2
    i ii Preface This Instrument Flying Handbook is designed for use by instrument flight instructors and pilots preparing for instrument rating tests. Instructors may find this handbook a valuable training aid as it includes basic reference material for knowledge testing and instrument flight training. Other Federal Aviation Administration (FAA) publications should be consulted for more detailed information on related topics. This handbook conforms to pilot training and certification concepts established by the FAA. There are different ways of teaching, as well as performing, flight procedures and maneuvers and many variations in the explanations of aerodynamic theories and principles. This handbook adopts selected methods and concepts for instrument flying. The discussion and explanations reflect the most commonly used practices and principles. Occasionally the word “must” or similar language is used where the desired action is deemed critical. The use of such language is not intended to add to, interpret, or relieve a duty imposed by Title 14 of the Code of Federal Regulations (14 CFR). All of the aeronautical knowledge and skills required to operate in instrument meteorological conditions (IMC) are detailed. Chapters are dedicated to human and aerodynamic factors affecting instrument flight, the flight instruments, attitude instrument flying for airplanes, basic flight maneuvers used in IMC, attitude instrument flying for helicopters, navigation systems, the National Airspace System (NAS), the air traffic control (ATC) system, instrument flight rules (IFR) flight procedures, and IFR emergencies. Clearance shorthand and an integrated instrument lesson guide are also included. This handbook supersedes Advisory Circular (AC) 61-27C, Instrument Flying Handbook, which was revised in 1980.
    [Show full text]
  • Flight Instruments - Rev
    Flight Instruments - rev. 9/12/07 Ground Lesson: Flight Instruments Objectives: 1. to understand the flight instruments, and the systems that drive them 2. to understand the pitot static system, and possible erroneous behavior 3. to understand the gyroscopic instruments 4. to understand the magnetic instrument, and the short comings of the instrument Justification: 1. understanding of flight instruments is critical to evaluating proper response in case of failure 2. knowledge of flight instruments is required for the private pilot checkride. Schedule: Activity Est. Time Ground 1.0 Total 1.0 Elements Ground: • overview • pitot-static instruments • gyroscopic instruments • magnetic instrument Completion Standards: 1. when the student exhibits knowledge relating to flight instruments including their failure symptoms 1 of 3 Flight Instruments - rev. 9/12/07 Presentation Ground: pitot-static system 1. overview (1) pitot-static system uses ram- air and static air measurements to produce readings. (2) pressure and temperature effect the altimeter i. remember - “Higher temp or pressure = Higher altitude” ii. altimeters are usually adjustable for non-standard temperatures via a window in the instrument (i) 1” of pressure difference is equal to approximately 1000’ of altitude difference 2. components (1) static ports (2) pitot tube (3) pitot heat (4) alternate static ports (5) instruments - altimeter, airspeed, VSI gyroscopic system 1. overview (1) vacuum :system to allow high-speed air to spin certain gyroscopic instruments (2) typically vacuum engine-driven for some instruments, AND electrically driven for other instruments, to allow back-up in case of system failure (3) gyroscopic principles: i. rigidity in space - gyroscopes remains in a fixed position in the plane in which it is spinning ii.
    [Show full text]
  • ASA Ch 3 the Instrument - Workbook Questions
    ASA Ch 3 The Instrument - Workbook Questions 1. The flight instruments are commonly grouped into basic categories based on the a. physical properties they rely on to work. b. whether they are used on the ground or in flight. c. Library of Congress catalog system, Dewey Decimal. 2. The basis of a conventional attitude indicator is a self-erecting a. vertical card mounted on a swivel. b. attitude flag arranged on a diagonal. c. gyroscope spinning on a vertical axis. 3. If the spin axis of the attitude indicator gyroscope moves off the vertical for some reason, the internal mechanism will realign it at a rate of approximately a. 3 degrees per second. b. 3 degrees per minute. c. 3 degrees per hour. 4. Occasionally, the miniature airplane on the attitude indicator may require repositioning while in level flight, due to changes in a. altitude (and corresponding air density). b. pitch attitude (associated with airspeed changes). c. the Earth’s gravitational forces. 5. If the attitude indicator experiences a failure of the power source, it will a. be unusable. b. continue to function if you maintain the same heading. c. still be a valid source of bank attitude. 6. Acceleration of the aircraft may cause the gyroscope to move off vertical, moving the horizon line a. toward the pilot. b. in the direction of the turn. c. to an incorrect position. 7. During a rapid acceleration, the horizon line will move down and the attitude indicator will indicate a false climb. a. True b. False 8. To avoid false indications when speeding up or slowing down, a pilot should increase the instrument scan rate a.
    [Show full text]
  • Finish Your Private Pilot License
    THE PRIVATE PILOT LEARNING GUIDE STOPPING A TURN CARDINAL DIRECTIONS Coordinated aileron and rudder pressure in the direction opposite When referencing the magnetic compass or heading indicator, always TURNS the bank will return the airplane to a level attitude. As with the associate one of the eight cardinal directions with the number on roll in the roll out of a bank attitude requires rudder deflection to the indicator. This will assist you in keeping spatially oriented and overcome adverse yaw. Relax elevator back pressure to return to a will be very important later in your training when you must visualize Rolling the airplane into a banked attitude results in a turn. Since the flight path is now curved there is an level pitch attitude as the bank attitude decreases. Neutralize the runway directions and while doing cross country navigation. controls when reaching a level sight picture. acceleration force. The increased force is directly related to the bank attitude used for the turn. A shallow As an aircraft rotates about its longitudinal axis, the lifting force bank attitude results in a slowly changing flight path, creating only a small increase in load factor. also rotates remaining perpendicular to the wingspan. When the airplane is in a bank, this redirected lift causes the airplane to turn. 60o As discussed earlier in this chapter, turning results in a curved flight path and additional load. The increase in load is due to centrifugal 40o force and is present anytime the airplane is turning. The centrifugal force combines with the airplane’s weight resulting in “load” opposite to lift.
    [Show full text]
  • The Inertial Navigation Unit: Teaching Navigation Principles Using a Custom Designed Sensor Package
    AC 2008-755: THE INERTIAL NAVIGATION UNIT: TEACHING NAVIGATION PRINCIPLES USING A CUSTOM DESIGNED SENSOR PACKAGE Joe Bradshaw, U.S. Naval Academy Electronics Technician at the US Naval Academy for the Weapons and Systems Engineering Department for 7 years. Design special hardware and develop software for projects and labs. Jack Nicholson, U.S. Naval Academy Page 13.1241.1 Page © American Society for Engineering Education, 2008 The Inertial Navigation Unit: Teaching Navigation Principles using a Custom Designed Sensor Package Abstract This paper describes the application and design of a small, inexpensive inertial navigation unit (INU) created to introduce systems engineering students at the United States Naval Academy (USNA) to the principles of navigation systems and to act as a navigation sensor for robotic and autonomous vehicle projects. The INU has been used in place of a multitude of standard navigation sensors such as an inertial measurement unit (IMU), magnetic compass module, and Global Positioning System (GPS) receiver. Its integrated design simplifies mechanical mounting, reduces navigation system weight and size, simplifies data interfacing with a control computer, and provides great flexibility for reconfiguring to meet a variety of engineering education objectives. The INU is capable of firmware upgrades and algorithm enhancements in the field via in-circuit programming, enhancing its longevity as a useful educational tool. In addition, a variety of controllers or a personal computer (PC) can communicate with the INU board through a standard RS-232C serial interface. This compact unit provides good system performance at a reasonable cost compared to most commercially available units. These features enable hands-on education techniques in the navigation aspects of robotics, examples of which are presented.
    [Show full text]
  • 1 Altimeter and Compass Watch Instruction Manual Overview Features • Hour, Minute, Second, Year, Month, Day, Day of Week •
    Altimeter and Compass Watch Instruction Manual Overview Figure 1 LCD display description Features • Hour, minute, second, year, • Auto calendar • 12/24 hour format display month, day, day of week • Daily alarm • Dual time • Stopwatch • Difference measurement of • Countdown timer • Altimeter – Barometer Use Altimeter and Barometer • 24 hour memory in • Logbook and logbook • 4 day memory in Barometer Altimeter history • Current absolute • Sea level pressure • Temperature display atmospheric • Electro – luminescent back • Compass • Low battery indicator lighted LCD • Diagnostics (System Reset) Care and Maintenance • Protect your watch from shocks, extreme heat and directly exposure to sunlight. • Don’t try to remove the housing or button of the watch. • Don’t insert any object into the watch. • Always put the watch in a clear, dry and room temperature environment when the watch is not used. • Follow the procedure discussed in the manual only. • Make sure the area around the sensors is free of dust or strong chemical. 1 Quick Reference Guide Figure 2 Quick Reference Guide 2 Time Time Main Mode Path Press (S1) until the mode indicator points to the “TIME” Field 1 Day of week, barometer trend indicator Field 2 Hour, Minute, Second Field 3 Month, day Second animation Outer Circumference Adjust o Hold (S2) for 1 second, the second digit will begin to flash o Press (S2) to select second minute hour 12/24hour year month day o Press (S3) or (S4) to set the function o Press (S1) to accept the setting Daily Alarm Path Press (S2) ×1 from Time Main Mode Field 1 “ON” or “OFF” Field 2 Time of a particular alarm Current time Field 3 Adjust o Press (S3) or (S4) to select the alarm number o Hold (S2) for 1 second, the “ON” or “OFF” will begin to flash o Press (S2) to select “ON” or “OFF” hour minute o Press (S3) or (S4) to set the function o Press (S1) to accept the setting Note “ ” will be displayed when any alarm is enabled.
    [Show full text]
  • 2016 Jeep Compass User's Guide
    Jeep.com (U.S.) Jeep.ca (Canada) DOWNLOAD A FREE ELECTRONIC COPY of the Owner’s Manual and Warranty Booklet by visiting: www.jeep.com/en/owners/manuals or www.jeep.com/en/warranty (U.S.); www.owners.mopar.ca/en (Canada). Jeep and Compass are registered trademarks of FCA US LLC. © 2015 FCA US LLC. All rights reserved. 16MK49-926-AA Compass First Edition User Guide 2016 COMPASS USER GUIDE 1888391_16a_Compass_UG_051315.indd 1 5/13/15 1:36 PM This guide has been prepared to help you get quickly acquainted with your new Jeep Brand Vehicle and to provide a convenient reference source for common questions. However, it is not a substitute for your Owner’s Manual. For complete operational instructions, maintenance procedures and important safety messages, please consult your Owner’s Manual, Navigation/Uconnect Manuals and other Warning Labels in your vehicle. If you are the first registered retail owner of your vehicle, you may obtain a complimentary printed copy of the Owner’s Not all features shown in this guide Manual, Navigation/Uconnect Manuals or Warranty Booklet by may apply to your vehicle. For additional information on accessories to help calling 1-877-426-5337 (U.S.) or 1-800-387-1143 (Canada) or personalize your vehicle, visit by contacting your dealer. www.mopar.com (U.S.), www.mopar.ca (Canada) or your local Jeep dealer. The driver’s primary the road. Use of any moving. If you find responsibility is the safe electrical devices, such as yourself unable to devote operation of the vehicle. cellular telephones, your full attention to Driving while distracted computers, portable vehicle operation, pull can result in loss of vehicle radios, vehicle navigation off the road to a safe control, resulting in a or other devices, by the location and stop your collision and personal driver while the vehicle is vehicle.
    [Show full text]
  • ½ Skydrop User Guide
    ½ SkyDrop user guide 2102 SkyDrop – combined GPS variometer instant analog/digital vario – no delay response GPS tracklog – IGC, FAI1 Civil approved or KML Bluetooth & USB connectivity – Android, iOS, PC full customizable – multiple screens, layouts and widgets xc navigation functions – optimized route for competitions thermal assistant, airspace warning, wind speed & direction ground speed, altitude above ground, compass, odometer light weight & compact size – 68g, 98 x 58 x 20 mm about this user guide Despite the fact that we made SkyDrop vario as intuitive as possible, we recommend to read this user guide. We know well this is not your favorite activity, so just briefly go through to understand basic concept. You can leave detailed study of every function for winter time or if you want to learn about specific function. You don’t have to keep the printed copy, PDF copy is stored inside vario (SD card), or you can find it on our webpage skybean.eu or vps.skybean.eu buttons long press (for 1s) – turn on, pull up menu bar, move to upper level in menu, toggle widget value, start/stop flight stopwatch, short press – confirm, list adjustable widgets on home screen, turn off device (if menu bar is pulled up), press & hold for 5s to turn device off short press – scroll between home screens to the left, select widget menu if menu bar is pulled up, scroll up in menu, lower value during setting parameter, press & hold to rapid value lowering short press – scroll between home screens to the right, select settings menu if menu bar is pulled up, scroll down in menu, raise value during setting parameter, press & hold to rapid value raising important note – please read SkyDrop is in silent mode after start-up, so if you want to hear vario sound, select FTime widget and manually start the flight by long press.
    [Show full text]
  • Blue Robotics Bluerov2bluerov2bluerov2 by Paul Unterweiser
    Tech File Blue Robotics BlueROV2BlueROV2BlueROV2 By Paul Unterweiser The popularity and availability of aerial quad-copter drones At fi rst glance, the BlueROV2 is a vectored six thruster ROV, have grown exponentially over the past few years. But, in capable of depths of 100 meters in a kit form. But because ev- large part because of the complexities that water penetration ery bit of the design, from the housings to thrusters to the fi rm- poses for electronics, underwater remotely operated vehicles ware that controls it, is open to the public, the future and up- (ROVs) have not experienced that same level of popularity. grade-ability of the design is virtually unlimited. This not only The technology required to fabricate the components for an means that people with technical skills will be able to adapt ROV to explore beyond a few meters depth has been beyond the BlueROV2 to perform whatever new tasks they might be the capabilities of all but a handful of companies who have clever enough to design, but it also means that even the aver- mastered the skills. In many cases, those skills have been age user is free to source parts and enhancements (such as kept proprietary and the products have demanded high prices. sonars) from whomever they want. This is an entirely new and Not long ago you needed well over $10,000 to consider buy- potentially powerful approach to ROV design and marketing. ing even the smallest observation ROV. As mini ROVs have grown in capabilities, so have the prices to the point where a What comes with the kit fully-capable mini ROV now costs in excess of $40,000.
    [Show full text]
  • Dash8-200/300 - Flight Instruments
    Dash8-200/300 - Flight Instruments FLIGHT INSTRUMENTS CONTROLS AND INDICATORS Left pilot’s instruments panel Page 1 Dash8-200/300 - Flight Instruments Right pilot’s instrument panel Page 2 Dash8-200/300 - Flight Instruments EADI EADI Attitude and heading reference system controller Page 3 Dash8-200/300 - Flight Instruments Airspeed indicator Page 4 Dash8-200/300 - Flight Instruments Primary altimeter Page 5 Dash8-200/300 - Flight Instruments Inertial vertical speed indicator with TCAS Page 6 Dash8-200/300 - Flight Instruments Radio magnetic indicator Page 7 Dash8-200/300 - Flight Instruments Stand-by attitude indicator Page 8 Dash8-200/300 - Flight Instruments IN MB 1021 Standby altimeter and standby magnetic compass Page 9 Dash8-200/300 - Flight Instruments or when button under glareshield is operated at the same time Davtron clock Page 10 Dash8-200/300 - Flight Instruments WX TERR EFIS controller Page 11 Dash8-200/300 - Flight Instruments WX TERR (WX/TERR) PUSH – displays (E)GPWS terrain map on the EHSI partial compass format PUSH – display will show EHSI data only, in partial compass format EFIS controller Page 12 Dash8-200/300 - Flight Instruments WX TERR EFIS controller Page 13 Dash8-200/300 - Flight Instruments Flight data recorder test switch Page 14 Dash8-200/300 - Flight Instruments Electronic Attitude Director Indicator (EADI) Page 15 Dash8-200/300 - Flight Instruments A LNAV or BC) Electronic Attitude Director Indicator (EADI) Page 16 Dash8-200/300 - Flight Instruments -- indicates active LNAV leg when selected Electronic Horizontal
    [Show full text]
  • ST-180 HSI Slaved Compass System Pilot's Operating Handbook
    ST-180 HSI Slaved Compass System Pilot’s Operating Handbook GPS HSI POH * Asterisk indicates pages changed, added, or deleted by List of Effective Pages revision. Retain this record in front of handbook. Upon receipt of a Record of Revisions revision, insert changes and complete table below. Revision Number Revision Date Insertion Date/Initials 1st Edition February 1992 2nd Edition March 05, 2002 2nd Ed: March 05, 2002 i HSI POH Page Intentionally Blank ii 2nd Ed: March 05, 2002 HSI POH Table of Contents Section Page 1.0 Introduction..............................................................................1-3 1.1 Notice.............................................................................1-3 2.0 Theory of Operation..................................................................2-3 2.1 General..........................................................................2-3 2.2 Horizontal Situation Indicator............................................2-3 2.3 Flux Sensor....................................................................2-4 2.4 Remote Gyro...................................................................2-4 2.5 Slaving Panel..................................................................2-4 2.6 Display Description..........................................................2-4 2.7 Indicators and Controls....................................................2-5 2.8 Slaving Panel..................................................................2-6 2.9 Indicators and Controls....................................................2-6
    [Show full text]