User manual
Table Of Contents
- Chapter 1 Introduction
- Chapter 2 Mechanical Description
- Chapter 3 Electronic Description
- Chapter 4 Maintenance and Storage
- Chapter 5 Operations
- Chapter 6 Launch and Recovery
- Chapter 7 MMP Firmware 4.X User Interface
- Figure 7-1: Electronics Board Configuration Error Message
- Power Up Sequence
- Re-Booting the System
- Prompts and Key Combinations
- Using the File Capture Utility
- Powering Down the MMP
- The Main Menu - Operating the MMP
- <1> Set Time
- <2> Diagnostics
- <3> Flash Card Ops
- <4> Sleep
- <5> Bench Test
- FSI CTD
- Sea-Bird CTD
- FSI ACM
- MAVS ACM
- Figure 7-36: MAVS ACM Pass-Through Communications
- Option <6> FSI ACM Tilt and Compass
- System Evaluation
- Option <7> Motor Operation
- Option <8> Brake On/Off Change?
- Option <9> Independent Watchdog
- System Options Tests
- Option Inductive Telemetry
- Option
Acoustic Transponder
- Option
Battery Endurance - Option
SIM/UIM Transactions - Option Inductive Charger Modem
- Option
Fluorometer - Option
CDOM Fluorometer - Option
IR Turbidity - Option Power UIM
- Option
Configure
- <6> Deploy Profiler
- Initialization
- Programming a Deployment
- MMP Deployment Definition Parameters
- Mooring ID
- Start Parameters
- Schedule Parameters
- Stops Parameters
- Endurance Parameters
- Deploy
- <7> Offload Deployment Data
- <8> Contacting McLane
Watchdog Initialization Profiling History Exiting to the Monitor
- Chapter 8 Data Offload, Processing, and Interpretation
- Overview
- Reviewing Deployment Data
- Removing the Flash Card
- Unpacking and Translating the Binary Data Files
- MMP Unpacker Application
- Editing MMPUnpacker.INI
- The PDP-N_NN Utility Program
- Processing and Interpreting MMP Data
- Mapping Velocity Measurements
- ACM Compass Calibration Step 1 – Map Horizontal C
- ACM Compass Calibration Step 2 – Plot Raw Measure
- ACM Compass Calibration Step 3 – Adjust Parameter
- ACM Compass Calibration Step 4 – Conduct a Spin T
- ACM Compass Calibration Step 5 – Removing the Bia
- Mapping Velocity Measurements to the Cartesian Earth Frame
- Sting and Acoustic Path Geometry
- Velocity Transformation
- Synchronizing the Data Streams
- Data Processing Shareware
- Appendix A Operating Crosscut for Windows and Crosscut
- Appendix B System Architecture
- Appendix C Bench Top Deployment
- Bench Top Deployment Example Settings
- Figure C-1: Bench top Deployment Example
- Figure C-2: Bench top Deployment Example (continued)
- Figure C-3: Bench top Deployment Example (continued)
- Figure C-4: Bench top Deployment Example (continued)
- Figure C-5:Bench top Deployment Example (continued)
- Figure C-6: Bench top Deployment Example (continued)
- Figure C-7: Bench top Deployment Example (continued)
- Figure C-8: Bench top Deployment Example (continued)
- Figure C-9: Bench top Deployment Example (continued)
- Figure C-10: Bench top Deployment Example (continued)
- Figure C-11: Bench top Deployment Example (continued)
- Figure C-12: Bench top Deployment Example (continued)
- Figure C-13: Bench top Deployment Example (continued)
- Figure C-14: Bench top Deployment Example (continued)
- Figure C-15 :Bench top Deployment Example (continued)
- Figure C-16: Bench top Deployment Example (continued)
- Figure C-17: Bench top Deployment Example (continued)
- Figure C-18: Bench top Deployment Example (continued)
- Figure C-19: Bench top Deployment Example (continued)
- Deployment Parameter Examples
- Bench Top Deployment Example Settings
- Appendix D ACM Compass Calibration
- Appendix E Optional Transponder
- Appendix F Unpacking data using PDP-N_NN.EXE
- Appendix G Rev C Electronics Board User Interface
- Power Up Sequence
- Re-Booting the System
- System Prompts and Key Combinations
- Using the File Capture Utility
- Powering Down the MMP
- The Main Menu - Operating the MMP
- <1> Set Time
- <2> Diagnostics
- <3> Flash Card Ops
- <4> Sleep
- <5> Bench Test
- Figure G-15: Bench Test
- Option <1> CTD Communication
- Verifying CTD Settings
- Option <2> CTD Pressure
- Option <3> CTD Average Pressure
- Option <4> CTD Temperature Record
- Option <5> ACM Communication
- Option <6> ACM Tilt and Compass
- Option <7> Motor Operation
- Option <8> Brake Set/Off Change?
- Option <9> Independent Watchdog
- System Options Tests
- Option Inductive Telemetry
- Option
Acoustic Transponder
- Option <0> Offload Routines
- Option
Fluorometer - Option
IR Turbidity - Option Power UIM
- <6> Deploy Profiler
- Programming a Deployment
- MMP Deployment Definition Parameters
- Mooring ID
- Start Parameters
- Schedule Parameters
- Stops Parameters
- Deploy
- Profile and Deployment Termination Conditions
- <7> Offload Deployment Data
- <8> Contacting McLane
Watchdog Initialization Profiling Odometer Exiting to the Monitor
- Appendix H Using the MMP Deployment Planner
- Creating a Deployment Plan
- Changing User Preferences
- Understanding Dive Zero
- Figure H-9: Deployment Planner Project Tab
- Figure H-10: Dive Zero - 1 Oct 2008, First Pattern 10 Oct 2008
- Figure H-11: Dive Zero - 1 Nov 2008, First Pattern 10 Oct 2009
- Figure H-12: Dive Zero - 20 Oct 2008, First Pattern Oct, 2008
- Figure H-13: Schedule Display in Profiler Firmware
- Figure H-14: Deployment Screen
- Figure H-15: Dive Zero Changed
- Appendix I Seapoint Analog Sensors
- Appendix J Underwater Inductive Modem (UIM)
- Appendix K Turbidity/Fluorometer Inductive Coil Configuration
- Appendix L Sea-Bird CTD Sensors
- Appendix M Aanderaa Oxygen Optode Sensor
- Appendix N MMP w/ Battery Housing Glass Sphere Extension
- Figure N-1: MMP with Battery Housing Glass Sphere Extension
- Figure N-2: MMP Battery Housing Glass Sphere Extension
- Figure N-3: Removing Bottom Bolts
- Figure N-4: Installed Support Legs
- Figure N-5: Removing Top Cap
- Figure N-6: Removing Horsehair Padding
- Figure N-7: Removing “Top” Sphere
- Figure N-8: Removing Panel Cap Screw
- Figure N-9: Installing Nylon Studs
- Figure N-10: Installing M3100A Extension Plate
- Figure N-11: Installing Front Panel Extension
- Figure N-12: Installing Spacer Legs with Studs
- Figure N-13: Reinstalling “Top” Sphere
- Figure N-14: Installing Spacer Legs with Studs
- Figure N-15: Frame Plate ‘A’ Reinstalled
- Figure N-16: Installing and Tightening Cap Screws on Front Panel
- Figure N-17: Tightening Cap Screw on Frame Plate
- Figure N-18: Glass Battery Housing Sphere Installed
- Figure N-19: Routed and Connected Cable
- Figure N-20: Installing Extension Skin
- Figure N-21: Reinstalling Horsehair
- Figure N-22: Reinstalling Top Cap
- Figure N-23: End Cap – Full View
- Figure N-24: Color-Coding on End Cap
hand indicated the positive direction of rotation.) Similarly, TY measures rotation about the x-
axis and is positive when the profiler tips to starboard. (Note that this rotation is consistent with
the "right-hand rule".) The units of tilt are degrees. Full scale for both pitch and roll is ±45°. Tilt
values near zero indicate that the profiler is vertical.
The next three numbers in each ACM scan are HX, HY, and HZ, the three components of
the local magnetic field as measured by the compass. Each component is normalized by the
strength of the magnetic field vector. Thus, for example,
222
hzhyhx
hx
HX
++
=
where hx, hy, and hz are the measured components of magnetic flux along each axis of the
compass. HY and HZ are determined similarly. Note that for the normalized values it is
necessarily true that HX
2
+ HY
2
+ HZ
2
= 1. The normalized values are also, by definition, the
direction cosines of the magnetic field in the frame of the MMP.
By convention the magnetic flux to be maximally positive along an axis of the compass is
defined when the magnetic field vector is parallel to that axis. The magnetic flux is maximally
negative along an axis of the compass when the magnetic field vector is anti-parallel to that axis.
The magnetic flux is zero along an axis of the compass when the magnetic field vector is
perpendicular to that axis. Using this convention see:
ϕ
sin
=
HZ
where φ is the angle of the magnetic field vector measured from the horizontal. φ is positive if
the field vector points above the horizontal and negative if it points below. Also there is:
HHorizontal
HHorizontal
HY
HYHX
HY
HX
HYHX
HX
θ
θ
cos
sin
22
22
==
+
==
+
Appendix D-5