Drop XML files in the browser to view.
Product_Observational
- Identification_Area
-
- logical_identifier
- urn:nasa:pds:maven.anc:data.drf.gnc:sci_anc_gnc14_341_342
- version_id
- 2.0
- title
- Guidance Navigation and Control DRF 2014-12-08
- information_model_version
- 1.13.0.0
- product_class
- Product_Observational
- Citation_Information
-
- publication_year
- 2020
- description
-
This is the Guidance Navigation and Control DRF file for 2014-12-08.
- Modification_History
-
- Modification_Detail
-
- modification_date
- 2020-08-18
- version_id
- 2.0
- description
-
The data file has been updated to correct header errors, remove data records at the beginning of the file which contained blank values, and remove truncated records at the end of data files.
- Observation_Area
-
- Time_Coordinates
-
- start_date_time
- 2014-12-08T03:20:19.328Z
- stop_date_time
- 2014-12-08T16:54:25.480Z
- Primary_Result_Summary
-
- purpose
- Engineering
- processing_level
- Raw
- Investigation_Area
-
- name
- Mars Atmosphere and Volatile EvolutioN
- type
- Mission
- Internal_Reference
-
- lid_reference
-
urn:nasa:pds:context:investigation:mission.maven
- reference_type
- data_to_investigation
- Observing_System
-
- Observing_System_Component
-
- name
- Mars Atmosphere and Volatile EvolutioN Mission
- type
- Spacecraft
- Internal_Reference
-
- lid_reference
-
urn:nasa:pds:context:instrument_host:spacecraft.maven
- reference_type
- is_instrument_host
- Target_Identification
-
- name
- Mars
- type
- Planet
- Internal_Reference
-
- lid_reference
-
urn:nasa:pds:context:target:planet.mars
- reference_type
- data_to_target
- Mission_Area
-
- MAVEN
-
- mission_phase_name
- Prime Mission
- File_Area_Observational
-
- File
-
- file_name
- sci_anc_gnc14_341_342.drf
- creation_date_time
- 2020-08-18T00:48:47
- file_size
- 5441475
- md5_checksum
- c920bca8037a93786b6ac46a55734466
- Header
-
- offset
- 0
- object_length
- 1300
- parsing_standard_id
- 7-Bit ASCII Text
- Table_Character
-
- offset
- 1300
- records
- 16739
- record_delimiter
- Carriage-Return Line-Feed
- Record_Character
-
- fields
- 24
- groups
- 0
- record_length
- 325
- Field_Character
-
- name
- SCET
- field_location
- 1
- data_type
- ASCII_String
- field_length
- 19
- Field_Character
-
- name
- ATT_QU_I2B_1 DN
- field_location
- 21
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The first element of current spacecraft attitude quaternion based on the current AD state running, phased as inertial to body.
- Field_Character
-
- name
- ATT_QU_I2B_2 DN
- field_location
- 34
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The second element of current spacecraft attitude quaternion based on the current AD state running, phased as inertial to body.
- Field_Character
-
- name
- ATT_QU_I2B_3 DN
- field_location
- 47
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The third element of current spacecraft attitude quaternion based on the current AD state running, phased as inertial to body.
- Field_Character
-
- name
- ATT_QU_I2B_4 DN
- field_location
- 60
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The four element of current spacecraft attitude quaternion based on the current AD state running, phased as inertial to body.
- Field_Character
-
- name
- ATT_QU_I2B_T DN
- field_location
- 73
- data_type
- ASCII_Real
- field_length
- 16
- unit
- DN
- description
-
ADS spacecraft time stamp (SCLK) of current spacecraft attitude quaternion based on the current AD state running, phased as inertial to body.
- Field_Character
-
- name
- ATT_RAT_BF_X DN
- field_location
- 90
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The current spacecraft angular X rate in the spacecraft body frame based on the current AD state running.
- Field_Character
-
- name
- ATT_RAT_BF_Y DN
- field_location
- 103
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The current spacecraft angular Y rate in the spacecraft body frame based on the current AD state running.
- Field_Character
-
- name
- ATT_RAT_BF_Z DN
- field_location
- 116
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The current spacecraft angular Z rate in the spacecraft body frame based on the current AD state running.
- Field_Character
-
- name
- APIG_ANGLE DN
- field_location
- 129
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The APP (articulated payload platform) measured inner gimbal axis angle for the sensor in use on the inner gimbal axis.
- Field_Character
-
- name
- APOG_ANGLE DN
- field_location
- 142
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The APP (articulated payload platform) measured outer gimbal axis angle for the sensor in use on the outer gimbal axis.
- Field_Character
-
- name
- APIG_APP_RAT DN
- field_location
- 155
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The measured APP (articulated payload platform) inner gimbal axis rate for the sensor in use on the inner gimbal axis.
- Field_Character
-
- name
- APOG_APP_RAT DN
- field_location
- 168
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The measured APP (articulated payload platform) outer gimbal axis rate for the sensor in use on the outer gimbal axis.
- Field_Character
-
- name
- RW1_SPD_DGTL DN
- field_location
- 181
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The reaction wheel rotational speed as determined by digital tachometer and filtered with a configurable digital speed filter. Data is returned in engineering units (rad/sec) and reflects both positive and negative rotation.
- Field_Character
-
- name
- RW2_SPD_DGTL DN
- field_location
- 194
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The reaction wheel rotational speed as determined by digital tachometer and filtered with a configurable digital speed filter. Data is returned in engineering units (rad/sec) and reflects both positive and negative rotation.
- Field_Character
-
- name
- RW3_SPD_DGTL DN
- field_location
- 207
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The reaction wheel rotational speed as determined by digital tachometer and filtered with a configurable digital speed filter. Data is returned in engineering units (rad/sec) and reflects both positive and negative rotation.
- Field_Character
-
- name
- RW4_SPD_DGTL DN
- field_location
- 220
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- description
-
The reaction wheel rotational speed as determined by digital tachometer and filtered with a configurable digital speed filter. Data is returned in engineering units (rad/sec) and reflects both positive and negative rotation.
- Field_Character
-
- name
- ACC_BOD_VECX DN
- field_location
- 233
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- Field_Character
-
- name
- ACC_BOD_VECY DN
- field_location
- 246
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- Field_Character
-
- name
- ACC_BOD_VECZ DN
- field_location
- 259
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- Field_Character
-
- name
- RW1_SPD_PTE DN
- field_location
- 272
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- Field_Character
-
- name
- RW2_SPD_PTE DN
- field_location
- 285
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- Field_Character
-
- name
- RW3_SPD_PTE DN
- field_location
- 298
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN
- Field_Character
-
- name
- RW4_SPD_PTE DN
- field_location
- 311
- data_type
- ASCII_Real
- field_length
- 12
- unit
- DN