## Voyager 1 Magnetometer Solar Wind Interplanetary Cruise Data Description  

ORIGINAL DATA_SET_NAME   
VOYAGER 1 SOLAR WIND MAGNETIC FIELD HGCOORDS 48SEC AVG V1.0 (VG1-SW-MAG-4-SUMM-HGCOORDS-48SEC-V1.0)   
VOYAGER 1 SOLAR WIND MAGNETIC FIELD HGCOORDS 1HR AVG V1.0 (VG1-SW-MAG-4-SUMM-HGCOORDS-1HR-V1.0)    
START_TIME = 1977-09-05       
STOP_TIME = 2004-12-31       
PDS3 DATA_SET_RELEASE_DATE = 2009-02-16     
PRODUCER_FULL_NAME = DR. LEONARD F. BURLAGA     

## PDS4 Collections
This document contains the data descriptions for the following collections:

- data-hg-1hr (urn:nasa:pds:vg1-mag-swind:data-hg-1hr)
- data-hg-48s (urn:nasa:pds:vg1-mag-swind:data-hg-48s)

## Collection Description

This document includes the Voyager 1 magnetometer solar wind data
from the interplanetary cruise averaged to 1 hour and 48 second samples in Heliographic 
coordinates.

## Confidence Level   

These data have been extracted from the NSSDC archive for distribution 
by the PDS along with other Voyager solar wind collections.  These data 
were not submitted to the PDS for archive and have not been through 
the PDS peer review process. These data are provided by the PDS for 
the convenience of PDS users.  Please exercise caution when using these data. 

At the time of experiment proposal, it was expected that the required 
accuracy of the measurements would be 0.1 nT, determined by the combined 
noise of the sensors and the spacecraft field. The spacecraft magnetic 
field at the outboard magnetic field sensor, referred to as the primary 
unit, was expected to be 0.2 nT and highly variable, consistent with 
current estimates. Hence, the [dual magnetometer design](https://doi.org/10.1029/JA076i016p03564).                                    
                                                                        
At distances > 40 AU, the heliospheric magnetic fields are generally 
and 85 AU is about 0.15 nT and 0.05 nT, respectively. The use of roll 
zero levels for the two independent magnetic axes that are perpendicular 
to the roll axis (which is nearly parallel to the radius vector to the 
Sun) at intervals of about 3 months. There is no roll calibration for 
the third magnetic axis. Comparison of the two derived magnetic vectors 
from the two magnetometers permits validation of the primary 
magnetometer data with an accuracy of 0.02 to 0.05 nT. A discussion of 
the uncertainties that must be considered when using these data is given 
in the Appendix A of [BURLAGAETAL2002](https://doi.org/10.1029/2001JA009217).                                                      
               
## Data Processing                                                            
                                                           
This data set contains hour averages of the interplanetary magnetic 
field (IMF) measurements obtained by the triaxial fluxgate magnetometer 
experiment on Voyager 1. Identical instruments on Voyager 1 and 2 were 
designed to measure the IMF between  Earth and Saturn (10 AU) during the 
primary Voyager mission. The  design and performance yielded absolute 
accuracies to better than < 0.1 nT. In general, each component of the 
hourly average has an uncertainty of up  to (+/- 0.05 nT) in the region 
beyond 10 AU. More accurate measurements can be obtained by special 
processing of the data, but it was not feasible to do this for the 
entire data set included here. The magnetic field magnitude in nT is 
provided along with angles of the field vector in the spacecraft-centered 
Heliographic (HG) coordinate system, also known as RTN.     

The high resolution data submitted to the NSSDC has its origins in the 
original MVS 'Summary' data sets formally produced on the NSSC IBM MVS 
mainframe system. The original data sets contain a mix of engineering, 
electron, magnetic field and plasma data. The Voyager magnetometer (MAG) 
experiment now resides on a dedicated workstation where only MAG  data are processed.

## Coordinate System                                                                                                                 
                                                                              
Interplanetary magnetic field studies make use of two important 
coordinate systems, the Inertial Heliographic (IHG) coordinate system 
and the Heliographic (HG) coordinate system. 
                                                                              
The IHG coordinate system is use to define the spacecraft's position. 
The IHG system is defined with its origin at the Sun. There are three 
orthogonal axes, X(IHG), Y(IHG), and Z(IHG). 

 - The Z(IHG) axis points northward along the Sun's spin axis.  
 - The X(IHG) - Y(IHG) plane lays in the solar equatorial plane. 
   
The intersection of the solar equatorial plane with the ecliptic plane 
defines a line, the longitude of the ascending node, which is taken to 
be the X(IHG) axis. The X(IHG) axis drifts slowly with time, approximately 
one degree per 72 years. 
                                                                              
Magnetic field orientation is defined in relation to the spacecraft. 
Drawing a line from the Sun's center (IHG origin) to the spacecraft 
defines the X axis of the HG coordinate system. 

The HG coordinate system is defined with its origin centered at the spacecraft. 
Three orthogonal axes are defined, X(HG), Y(HG), and Z(HG). 

 - The X(HG) axis  points radially away from the Sun
 - The Y(HG) axis is parallel to the solar equatorial plane and therefore parallel to the X(IHG)-Y(IHG) plane.  
 - The Z(HG) axis is chosen to complete the orthonormal triad.        
                                                                              
A reference guide with diagrams explaining the IHG and HG systems may be found in Space and Science Reviews, Volume 39 (1984), pages 255-316, [MHD Processes in the Outer Heliosphere](https://doi.org/10.1007/BF00173902), L. F. Burlaga. 
                                        
## 48 Second Averaged Data Format   

The data consists of the following columns:

1. s/c identification (FLT1=Voyager 1) (FLT2=Voyager 2)                               
2. coordinate system  (HG=heliographic)used for this data set        
3. Time (UTC) format                             
4. field magnitude (nT)                                              
5. field component 1 (nT) - HG                                       
6. field component 2 (nT) - HG                                       
7. field component 3 (nT) - HG                                       
8. spacecraft radial distance (AU)                                   
9. spacecraft x position (AU) - IHG                                  
10. spacecraft y position (AU) - IHG                                  
11. spacecraft z position (AU) - IHG  

## 1 hour Averaged Data Format

The data consist in two formats described below:

### Data before 1990 
1. s/c identification (FLT1=Voyager 1) (FLT2=Voyager 2)                                      
2. Time (UTC) format      
3. X IHG position component (A.U. - IHG coordinates)             
4. Y IHG position component (A.U. - IHG coordinates)             
5. Z IHG position component (A.U. - IHG coordinates)
6. Heliocentric Range = sqrt(X*X + Y*Y+Z*Z)        
7. Field 1 Magnitude (nT)  (avg(F2(48sec)))      
8. Field 2 modulus (nT)  norm (B1,B2,B3)        
9. Delta Latitudinal angle (degrees - HG coordinates)  
10. Lambda Longitudinal angle (degrees - HG coordinates)  

### Data after 1990 
1. s/c identification (FLT1=Voyager 1) (FLT2=Voyager 2)                                      
2. Time (UTC) decimal year format      
3. The magnetic field strength, F1, computed from high-resolution observations            
4. The elevation angle (degrees) in heliographic coordinates            
5. The azimuthal angle (degrees) in heliographic coordinates
6. The magnetic field strength, F2, computed from hour              
               averages of the components. The components of B can be         
               computed from F2 and the two angles. 
                                                                              
## Acknowledgement                                                                                                                        

Use of these data in publications should be accompanied at minimum by 
acknowledgements of the National Space Science Data Center and the 
responsible Principal Investigator defined in the experiment documentation.                                            
