Detail Supported Instruments (#478)

* Initial changes and additions to specify validated cameras

* Addressed PR feedback

* Missed a couple acronyms in LRO rst file

* Fixed title underline in LRO

docs/source/sensors/Odyssey.rst

-Odyssey THEMIS IR
-=================
-The Thermal Emission Imaging System Infrared sensor is a linescan camera
+Odyssey Thermal Emission Imaging System Infrared
+================================================
+The Thermal Emission Imaging System (THEMIS) Infrared sensor (IR) is a linescan camera
 responsible for capturing 10 infrared bands at a spatial resolution of 100
 meters per pixel.
 
@@ -8,9 +8,9 @@ meters per pixel.
 Processing THEMIS IR Images
 ---------------------------
 
-Odyssey THEMIS VIS
-==================
-The Thermal Emission Imaging System Visible sensor is a push frame camera
+Odyssey Thermal Emission Imaging System Visible
+===============================================
+The Thermal Emission Imaging System (THEMIS) Visible sensor (VIS) is a push frame camera
 responsible for capturing 5 color bands at a spatial resolution of 18 meters
 per pixel.
 

docs/source/sensors/OsirisRex.rst

+OsirisRex SamCam
+================
+
+OsirisRex PolyCam
+=================
+
+OsirisRex NavCam
+================
\ No newline at end of file

docs/source/sensors/Rosetta.rst

+Rosetta Visible and Infrared Thermal Imaging Spectrometer
+=========================================================
\ No newline at end of file

docs/source/sensors/TraceGasOrbiter.rst

-TGO CaSSIS
-==========
-The Trace Gas Orbiter's Color and Stereo Surface Imaging System is a 4 filter
+TGO Color and Stereo Surface Imaging System
+===========================================
+The Trace Gas Orbiter's Color and Stereo Surface Imaging System (CaSSIS) is a 4 filter
 frame camera capable of capturing data at a resolution of 4.6 meters per pixel.
 The camera is mounted on a rotating mechanism, and it is able to capture stereo
 imagery in a single pass.

docs/source/sensors/Voyager.rst

-Voyager
-=======
+Voyager Wide/Narrow Angle Camera
+================================
 The voyager imaging system is a set of two instruments -- a wide angle camera
 (WAC) and a narrow angle camera (NAC).  The wide angle camera contains 8 filters
 and has a field of view of 3.2 degrees.  The narrow angle camera also contains 8

docs/source/sensors/index.rst

@@ -4,17 +4,40 @@ Cameras that can be used with USGSCSM
 
 .. toctree::
   Cassini
-  Dawn
-  Galileo
-  Hayabusa
-  Juno
   LunarReconnaissanceOrbiter
   MarsExpress
   MarsReconnaissanceOrbiter
   Messenger
+  Kaguya
+
+##############################################
+Available Cameras that have not been evaluated
+##############################################
+
+If there is a camera on this list that you would like to be verified for use
+please make an issue_ and we will get to the evaluation in a timely manner
+
+.. toctree::
+  Apollo
+  Chandrayaan
+  Clementine
+  Clipper
+  Dawn
+  Galileo
+  Hayabusa
+  Hayabusa2
+  Juno
+  LunarOrbiter
+  Mariner10
+  MarsGlobalSurveyor
+  Near
+  MarsScienceLaboritory
   NewHorizons
   Odyssey
-  Selene
+  OsirisRex
+  Rosetta
   TraceGasOrbiter
   Viking
   Voyager
+
+.. _issue: https://github.com/USGS-Astrogeology/usgscsm/issues?state=open
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