PDS_VERSION_ID = PDS3 RECORD_TYPE = STREAM OBJECT = TEXT PUBLICATION_DATE = 2000-04-10 NOTE = "PLS sector description." END_OBJECT = TEXT END Table 7. AACS Sector ID Sectoring mode AACS Sector values -------------------- ------------------------------------- Quadrants (4/spin) 0, 64, 128, 192 Octants (8/spin) 0, 32, 64, 96, 128, 160, 192, 224 The AACS rotor spin angle is an integer number in the range 0-255. It is zero when the spacecraft X-axis is pointed at (or near) the south ecliptic pole and increases as the spacecraft rotates. The rotor spin angle may be converted to an angle in the range 0-360 degrees with the equation: angle = (AACS rotor spin angle) * (360/256) The fields-of-view of the PLS detectors are offset by 45 degrees from the spacecraft X-axis in the X-Y plane. So when the rotor spin angle is zero (0) the fields-of-view are making a +45 degree angle with respect to the X-axis in the X-Y plane. This 45 degree offset is not included in the AACS rotor spin angle provided in the RDR data files. To compute the rotational angle from the north ecliptic pole to the velocity vector of the plasma particles entering the PLS field-of-view: velocity angle = 45 + [ (AACS rotor spin angle) * (360/256) ] A significant challenge to the PLS flight software was decoupling data collection from data transmission. Plasma measurements need strong control of, and repeatability in, the angular sampling. A very conscious trade was made by the PLS team to relax the time knowledge in favor of tightening the angular knowledge. This means that the PLS data can not be directly compared to the spacecraft attitude (AACS) data set based solely on the time word. PLS uses the AACS CLOCK data distributed onboard the spacecraft to determine when to begin accumulating sensor data. Depending on the modes of operation PLS may begin, for example, on quadrant or octant sector boundaries. Within each sector the instrument uses a fixed accumulation time for each sample. Thus within each sector successive samples (successive energy steps) start at successively larger angles as the spacecraft rotates at ~18.9 degrees/second. The time assigned to each measurement in an RDR file is the time that data collection was initiated for that particular mode. Thus, data collected over approximately one spin of the spacecraft will all have the same SCLK time in the file. And since the actual data collection begins on a sector boundary, the actual time of the first data may be up to one sector later than the initiation time.