[nasa/nos3#181] - Update submodule for new inertial attitude control …

[msuder]

…mode.

Depends on submodule pull request nasa-itc/generic_adcs#9 .

Closes #181.

[msuder]

How to test:

Launch NOS3 as normal using COSMOS as the GSW.
GENERIC_STAR_TRACKER GENERIC_STAR_TRACKER_ENABLE_CC
GENERIC_ADCS GENERIC_ADCS_INERTIAL_QUATERNION_CC with GNC_INER_QUAT1 0.0, GNC_INER_QUAT2 0.0, GNC_INER_QUAT3 0.0, GNC_INER_QUAT4 1.0
GENERIC_ADCS GENERIC_ADCS_SET_MODE_CC with GNC_MODE INERTIAL_MODE

Watch telemetry page
GENERIC_ADCS GENERIC_ADCS_AC

Look at telemetry point INERTIAL_QUAT_ERR_3. It should gradually move towards 0.99999. When it does, the inertial attitude matches the commanded inertial attitude. You can also look at the 42 Cam window; turn on the N and B axes and see that b1 aligns with n1, b2 aligns with n2, b3 aligns with n3.

Note that the star tracker must be returning valid data for this to work. To see if it is, look at telemetry point
GENERIC_ADCS GENERIC_ADCS_AD ST_VALID.

[jlucas9]

Standard boot with COSMOS GSW.
cmd("GENERIC_STAR_TRACKER GENERIC_STAR_TRACKER_ENABLE_CC")

Successfully sun pointed by default:

cmd("GENERIC_ADCS GENERIC_ADCS_INERTIAL_QUATERNION_CC with GNC_INER_QUAT1 0.0, GNC_INER_QUAT2 0.0, GNC_INER_QUAT3 0.0, GNC_INER_QUAT4 1.0")
cmd("GENERIC_ADCS GENERIC_ADCS_SET_MODE_CC with GNC_MODE INERTIAL_MODE")

Confirmed telemetry in inertial mode (maintained for awhile too):

[dacarter22]

Intertial_quart_err_3 approaches 0.9999999 repeating

[zlynch2]

Confirmed we were in adcs mode 3, also confirmed the Qerror approaches 1. Also confirmed the axis match as described. Approving.