diff --git a/docs/source/sensors/Apollo.rst b/docs/source/sensors/Apollo.rst
new file mode 100644
index 0000000000000000000000000000000000000000..cef1fc59d3a185b7c2270aa1df289798b8cbeaa0
--- /dev/null
+++ b/docs/source/sensors/Apollo.rst
@@ -0,0 +1,2 @@
+Apollo Metric
+=============
\ No newline at end of file
diff --git a/docs/source/sensors/Cassini.rst b/docs/source/sensors/Cassini.rst
index a8f586cde15659535d677151e2b605a0def0b4b8..ce7acc77ffde490d8a4efff0317a7f42bde992fd 100644
--- a/docs/source/sensors/Cassini.rst
+++ b/docs/source/sensors/Cassini.rst
@@ -1,6 +1,6 @@
-Cassini ISS
-===========
-The Cassini Imaging Subsystem comprises two instruments -- a narrow angle camera
+Cassini Imaging Subsystem
+=========================
+The Cassini Imaging Subsystem (ISS) comprises two instruments -- a narrow angle camera
and a wide angle camera. The narrow angle camera contains 24 filters, and the
wide angle camera contains 18 filters.
diff --git a/docs/source/sensors/Chandrayaan.rst b/docs/source/sensors/Chandrayaan.rst
new file mode 100644
index 0000000000000000000000000000000000000000..d72a70b93234eceb9db094795daf01c79b31b5be
--- /dev/null
+++ b/docs/source/sensors/Chandrayaan.rst
@@ -0,0 +1,5 @@
+Chandrayaan1 Moon Mineralogy Mapper
+===================================
+
+Chandrayaan1 Forerunner
+=======================
\ No newline at end of file
diff --git a/docs/source/sensors/Clementine.rst b/docs/source/sensors/Clementine.rst
new file mode 100644
index 0000000000000000000000000000000000000000..6f8084cae997d2086e85297ef5febec4f98b2464
--- /dev/null
+++ b/docs/source/sensors/Clementine.rst
@@ -0,0 +1,11 @@
+Clementine Ultraviolet/Visible
+==============================
+
+Clementine Near-Infrared
+========================
+
+Clementine High-Resolution
+==========================
+
+Clementine Long-Wave Infrared
+=============================
\ No newline at end of file
diff --git a/docs/source/sensors/Clipper.rst b/docs/source/sensors/Clipper.rst
new file mode 100644
index 0000000000000000000000000000000000000000..17507dfbfa4c956dbb29d6c244094d3ec402f97f
--- /dev/null
+++ b/docs/source/sensors/Clipper.rst
@@ -0,0 +1,2 @@
+Clipper Europa Imaging System
+=============================
\ No newline at end of file
diff --git a/docs/source/sensors/Dawn.rst b/docs/source/sensors/Dawn.rst
index 51cde4b631acec75140b3627312ada0341070dc4..4332a51f89bb354bf0104782b1280d106efb9255 100644
--- a/docs/source/sensors/Dawn.rst
+++ b/docs/source/sensors/Dawn.rst
@@ -1,6 +1,6 @@
-Dawn FC
-=======
-The Dawn Framing Camera is a frame camera with a resolution of up to 25 meters
+Dawn Framing Camera
+===================
+The Dawn Framing Camera (FC) is a frame camera with a resolution of up to 25 meters
per pixel. This instrument contains a clear filter and 7 band-pass filters.
Processing Dawn FC Images
diff --git a/docs/source/sensors/Galileo.rst b/docs/source/sensors/Galileo.rst
index 9de137cb86d3f544b2b232c85527ad37f721d023..9e92c2697a9da946b52628566061604b00654486 100644
--- a/docs/source/sensors/Galileo.rst
+++ b/docs/source/sensors/Galileo.rst
@@ -1,6 +1,6 @@
-Galileo SSI
-===========
-The Galileo Solid State Imager is a modified form of the Voyager Narrow Angle
+Galileo Solid State Imager
+==========================
+The Galileo Solid State Imager (SSI) is a modified form of the Voyager Narrow Angle
Camera. Galileo SSI has 8 band filters and is capable of capturing imagery with
a spatial resolution up to 1 kilometer per pixel.
diff --git a/docs/source/sensors/Hayabusa.rst b/docs/source/sensors/Hayabusa.rst
index d6d8d4bd3d434b2d09ee7a6531ee11cb6fa4ccca..bd92ad27abf5b7689f690414ade2a69006ee0213 100644
--- a/docs/source/sensors/Hayabusa.rst
+++ b/docs/source/sensors/Hayabusa.rst
@@ -1,9 +1,5 @@
-Hayabusa ONC
-============
-The Hayabusa Optical Navigation Camera is suite of three instruments (two wide
-angle and one telescopic imager), and is primarily used for navigation. The
-wide angle cameras employ clear filters, and the telescopic imager uses 7
-color filters and one clear filter.
+Hayabusa Asteroid Multi-band Imaging Camera
+===========================================
-Processing Hayabusa ONC Images
-------------------------------
+Hayabusa Near Infrared Spectrometer
+===================================
diff --git a/docs/source/sensors/Hayabusa2.rst b/docs/source/sensors/Hayabusa2.rst
new file mode 100644
index 0000000000000000000000000000000000000000..2bd36c71a58d161eb3154be749504578e717677c
--- /dev/null
+++ b/docs/source/sensors/Hayabusa2.rst
@@ -0,0 +1,9 @@
+Hayabusa2 Optical Navigation Camera
+===================================
+The Hayabusa2 Optical Navigation (ONC) Camera is suite of three instruments (two wide
+angle and one telescopic imager), and is primarily used for navigation. The
+wide angle cameras employ clear filters, and the telescopic imager uses 7
+color filters and one clear filter.
+
+Processing Hayabusa2 ONC Images
+-------------------------------
\ No newline at end of file
diff --git a/docs/source/sensors/Selene.rst b/docs/source/sensors/Kaguya.rst
similarity index 83%
rename from docs/source/sensors/Selene.rst
rename to docs/source/sensors/Kaguya.rst
index 64de671f46c3cd055d4c1e5d94b7771160b3aff8..3fa2f9562f4e8005f6c86ca280f26cd81953ed80 100644
--- a/docs/source/sensors/Selene.rst
+++ b/docs/source/sensors/Kaguya.rst
@@ -1,6 +1,6 @@
-Kaguya TC
-=========
-The Kaguya Terrain Camera is a dual-band, stereo, linescan camera with a spatial
+Kaguya Terrain Camera
+=====================
+The Kaguya Terrain Camera (TC) is a dual-band, stereo, linescan camera with a spatial
resolution of 20 meters per pixel. This set of sensors uses two telescopic
imaging instruments, one pointed forward, and one pointed backward. Together,
these instruments provide data necessary to create stereoscopic imagery.
@@ -37,9 +37,9 @@ Begin by generating an ISD as described in the section on :ref:`isd_generation`.
isd = csmapi.Isd(alelabel)
camera = plugin.constructModelFromISD(isd, model)
-Kaguya MI
-=========
-The Kaguya Multiband Imagery platform comprises two different instruments -- a
+Kaguya Multiband Imagery platform
+=================================
+The Kaguya Multiband Imagery (MI) platform comprises two different instruments -- a
visible light sensor (VIS) and a near infrared sensor (NIR). The visible light
sensor has a spatial resolution of 20 meters per pixel, and collects 5 bands of
data via a bandpass filter. The near infrared sensor is responsible for
diff --git a/docs/source/sensors/LunarOrbiter.rst b/docs/source/sensors/LunarOrbiter.rst
new file mode 100644
index 0000000000000000000000000000000000000000..0ff257760e8a2134707e17c8359f78f03eacb742
--- /dev/null
+++ b/docs/source/sensors/LunarOrbiter.rst
@@ -0,0 +1,2 @@
+LunarOrbiter High Camera
+========================
\ No newline at end of file
diff --git a/docs/source/sensors/LunarReconnaissanceOrbiter.rst b/docs/source/sensors/LunarReconnaissanceOrbiter.rst
index 168e9df215ba0551b76ebc055d163b5ceedf816d..3048da7f5bfe174108161af8979e249c766e133a 100644
--- a/docs/source/sensors/LunarReconnaissanceOrbiter.rst
+++ b/docs/source/sensors/LunarReconnaissanceOrbiter.rst
@@ -1,25 +1,25 @@
-MiniRF
-======
-MiniRF is the Lunar Reconnaissance Orbiter's Miniature Radio Frequency instrument.
-This instrument features two wavelength bands, and has a resolution of 30 meters
+Lunar Reconnaissance Orbiter Miniature Radio-Frequency
+======================================================
+Lunar Reconnaissance Orbiter (LRO) Miniature Radio Frequency (MiniRF) instrument
+features two wavelength bands, and has a resolution of 30 meters
per pixel.
Processing MiniRF Images
------------------------
-LRO NAC
-=======
-LRO NAC is the Lunar Reconnaissance Orbiter's Narrow Angle Camera. It is a
+Lunar Reconnaissance Orbiter Narrow Angle Camera
+================================================
+Lunar Reconnaissance Orbiter (LRO) Narrow Angle Camera (NAC) is a
panchromatic linescan imager with a resolution of .5 meters per pixel over a 5km
swath.
Processing LRO NAC Images
-------------------------
-LRO WAC
-=======
-LRO WAC is the Lunar Reconnaissance Orbiter's Wide Angle Camera. This is a
+Lunar Reconnaissance Orbiter Wide Angle Camera
+==============================================
+Lunar Reconnaissance Orbiter (LRO) Wide Angle Camera (WAC) is a
pushframe camera with a resolution of 100 meters per pixel over a 65km swath.
This instrument captures data in 7 bands.
diff --git a/docs/source/sensors/Mariner10.rst b/docs/source/sensors/Mariner10.rst
new file mode 100644
index 0000000000000000000000000000000000000000..5a38540707f8452b1b02d95addde36e4cd6d3109
--- /dev/null
+++ b/docs/source/sensors/Mariner10.rst
@@ -0,0 +1,2 @@
+Mariner10
+=========
\ No newline at end of file
diff --git a/docs/source/sensors/MarsExpress.rst b/docs/source/sensors/MarsExpress.rst
index 96e037f99c066d23017fc9f3473cd02c95ccb342..a7ff650c3b865c3daf56986ceb35100c56183f2e 100644
--- a/docs/source/sensors/MarsExpress.rst
+++ b/docs/source/sensors/MarsExpress.rst
@@ -1,8 +1,8 @@
-MEX HRSC
-========
-* HRSC has 9 different filters. Each has it's own instrument id, as well as
+Mars Express High Resolution Stereo Camera
+==========================================
+* High Resolution Stereo Camera (HRSC) has 9 different filters. Each has it's own instrument id, as well as
the main/"HEAD" camera composing those filters. There is also another
- "SRC" channel, making-up a total of 11 distinct sensors. It is very
+ "Super-Resolution Channel" (SRC) channel, making-up a total of 11 distinct sensors. It is very
important to understand which code is needed when/where.
* HRSC is a variable rate line scanner, and so does not maintain one exposure
diff --git a/docs/source/sensors/MarsGlobalSurveyor.rst b/docs/source/sensors/MarsGlobalSurveyor.rst
new file mode 100644
index 0000000000000000000000000000000000000000..1e24e3e3c2c801cad0a50f7bea87fb03aa69b534
--- /dev/null
+++ b/docs/source/sensors/MarsGlobalSurveyor.rst
@@ -0,0 +1,5 @@
+MarsGlobalSurveyor Mars Orbiter Camera Wide Angle Camera
+========================================================
+
+MarsGlobalSurveyor Mars Orbiter Camera Narrow Angle Camera
+==========================================================
\ No newline at end of file
diff --git a/docs/source/sensors/MarsReconnaissanceOrbiter.rst b/docs/source/sensors/MarsReconnaissanceOrbiter.rst
index 41b35096a854197db042aa068483d8c5bc5758ad..1198d92074de0a28d5ef5d7e2410c3781fb886d1 100644
--- a/docs/source/sensors/MarsReconnaissanceOrbiter.rst
+++ b/docs/source/sensors/MarsReconnaissanceOrbiter.rst
@@ -1,9 +1,21 @@
-MRO CTX
-=======
-The Mars Reconnaissance Orbiter Context Camera (CTX) is a high resolution linescan
+Mars Reconnaissance Orbiter Context Camera
+==========================================
+The Mars Reconnaissance Orbiter (MRO) Context Camera (CTX) is a high resolution linescan
imager that is capable of capturing grayscale images with a resolution of up to
6 meters per pixel.
Processing MRO CTX Images
-------------------------
+
+Mars Reconnaissance Orbiter High Resolution Imaging Science Experiment
+======================================================================
+
+Processing MRO HiRISE Images
+----------------------------
+
+Mars Reconnaissance Orbiter Mars Color Imager
+=============================================
+
+Processing MRO Marci Images
+---------------------------
diff --git a/docs/source/sensors/MarsScienceLaboritory.rst b/docs/source/sensors/MarsScienceLaboritory.rst
new file mode 100644
index 0000000000000000000000000000000000000000..eef2c0258fca53cd4f49c2d46baafd580f571a55
--- /dev/null
+++ b/docs/source/sensors/MarsScienceLaboritory.rst
@@ -0,0 +1,5 @@
+Mars Science Laboritory Mast Camera
+===================================
+
+Mars Science Laboritory Navigation Camera
+=========================================
\ No newline at end of file
diff --git a/docs/source/sensors/Messenger.rst b/docs/source/sensors/Messenger.rst
index a59f668dd5efaba91fb605a0d83da897223525d5..8664845255e0d79b7a673f668d07838f2f182f6f 100644
--- a/docs/source/sensors/Messenger.rst
+++ b/docs/source/sensors/Messenger.rst
@@ -1,5 +1,5 @@
-Messenger MDIS
-==============
+Messenger Dual Imaging System
+=============================
The Messenger Mercury Dual Imaging System (MDIS) is a suite of two framing
cameras-- a wide angle camera (WAC) and a narrow angle camera (NAC). The wide
angle camera captures multispectral information, and the narrow angle camera
diff --git a/docs/source/sensors/Near.rst b/docs/source/sensors/Near.rst
new file mode 100644
index 0000000000000000000000000000000000000000..96ec03656f2d1d0395528af0fecd3a93c28d4049
--- /dev/null
+++ b/docs/source/sensors/Near.rst
@@ -0,0 +1,2 @@
+Near MultiSpectral Imager
+=========================
\ No newline at end of file
diff --git a/docs/source/sensors/NewHorizons.rst b/docs/source/sensors/NewHorizons.rst
index 2a443439fb3d9567d508157f498ac74d1bff40dc..6146845e50905bb67a7f681a88c913739e05f4c9 100644
--- a/docs/source/sensors/NewHorizons.rst
+++ b/docs/source/sensors/NewHorizons.rst
@@ -1,6 +1,6 @@
-New Horizons LORRI
-==================
-New Horizons Long Range Reconnaissance Imager is a fixed, narrow angle frame
+New Horizons Long Range Reconnaissance Imager
+=============================================
+New Horizons Long Range Reconnaissance Imager (LORRI) is a fixed, narrow angle frame
camera with a field of view of .29 degrees. LORRI is a panchromatic imaging
system, and it offers a maximum spatial resolution of roughly 33 meters per
pixel.
diff --git a/docs/source/sensors/Odyssey.rst b/docs/source/sensors/Odyssey.rst
index cf74fd36f3614f37bccbefd8deafb4546de28813..22ecbcbcfc2c3b2007afd3e5f9c5e7aee20f7682 100644
--- a/docs/source/sensors/Odyssey.rst
+++ b/docs/source/sensors/Odyssey.rst
@@ -1,6 +1,6 @@
-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.
diff --git a/docs/source/sensors/OsirisRex.rst b/docs/source/sensors/OsirisRex.rst
new file mode 100644
index 0000000000000000000000000000000000000000..b731107f1acf1bb7c778a1976a13022637268098
--- /dev/null
+++ b/docs/source/sensors/OsirisRex.rst
@@ -0,0 +1,8 @@
+OsirisRex SamCam
+================
+
+OsirisRex PolyCam
+=================
+
+OsirisRex NavCam
+================
\ No newline at end of file
diff --git a/docs/source/sensors/Rosetta.rst b/docs/source/sensors/Rosetta.rst
new file mode 100644
index 0000000000000000000000000000000000000000..e8aa2eae6f5338fb020c520d88f83bf5bf783b28
--- /dev/null
+++ b/docs/source/sensors/Rosetta.rst
@@ -0,0 +1,2 @@
+Rosetta Visible and Infrared Thermal Imaging Spectrometer
+=========================================================
\ No newline at end of file
diff --git a/docs/source/sensors/TraceGasOrbiter.rst b/docs/source/sensors/TraceGasOrbiter.rst
index 147fb5b2925d23aa3285ca68f4708b5e3d4ea325..9922f3eb254f44e0ccccdfbf6df423938117035e 100644
--- a/docs/source/sensors/TraceGasOrbiter.rst
+++ b/docs/source/sensors/TraceGasOrbiter.rst
@@ -1,6 +1,6 @@
-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.
diff --git a/docs/source/sensors/Voyager.rst b/docs/source/sensors/Voyager.rst
index 3407df33d909e80bfe07298d5dc14b12872188af..e5359feead6bae5c85765c1666e5967c69d94b3e 100644
--- a/docs/source/sensors/Voyager.rst
+++ b/docs/source/sensors/Voyager.rst
@@ -1,5 +1,5 @@
-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
diff --git a/docs/source/sensors/index.rst b/docs/source/sensors/index.rst
index 5355a133991b96ce0efccda3eaab2fcca57bb6f5..600d81d0624d3107f6b3594bbe7b25f311fda609 100644
--- a/docs/source/sensors/index.rst
+++ b/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
\ No newline at end of file