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
The bias angles are simple additive errors to the sting heading angle, θ
H
(it is the total bias
that is of concern, so it is unnecessary to differentiate between the two sources). To measure the
total, measure the difference between the heading calculated using MX and MY, the offset and
scale corrected measurements, and the true heading, as measured using the hand compass.
Consider this expression for the sting heading angle in a true north Cartesian earth frame:
DevPMCH
MBBB
MY
MX
++++
=
−1
tan
θ
M
DEV
is the magnetic deviation, the bearing of magnetic north measured from true north in
mathematical compass coordinates. M
DEV
is positive in the North Atlantic and negative in the
North Pacific. B
P
is the error between the actual magnetic bearing of the sting and the target
magnetic bearing during the spin test. M
DEV
for any location on the earth can be looked up in a
reference and used to correct the heading angle. The total bias angle, B
T
= B
C
+ B
M
, can be
measured, but the accuracy of that measurement is limited by the magnitude of B
P
. This is why
good alignment of the sting using the hand compass is a critical part of the spin test. A good
alignment means that B
P
is negligibly small, leaving us with:
DEVTH
MB
MY
MX
++
=
−1
tan
θ
Working in the magnetic or compass frame, B
T
can be measured at each of the eight
cardinal points of the compass:
−=
−
MY
MX
B
HT
1
tan
θ
θ
H
is the actual magnetic bearing in mathematical compass coordinates (90° for magnetic north,
45° for magnetic northeast, 0° for magnetic east, etc.). MX and MY are derived from the raw
measurements and the corrections obtained by mapping those measurements to the unit circle.
You can perform this calculation with a hand calculator, or use the Nelder-Mead simplex
minimization provided by McLane. The calculation of B
T
at the eight cardinal points is triggered
whenever the raw data being processed include exactly eight elements in a file named
SPINTEST.TXT. The calculation assumes the data are in north, northeast, east, southeast, south,
southwest, west, northwest order.
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