During the extended science phase of the Mars Reconnaissance Orbiter's lifecycle, the operational duties pertaining to navigation primarily involve orbit determination. The orbit determination process utilizes radiometric tracking data and is used for the prediction and reconstruction of MRO's trajectories. Predictions are done twice per week for ephemeris updates on-board the spacecraft and for planning purposes. Orbit Trim Maneuvers (OTM-s) are also designed using the predicted trajectory. Reconstructions, which incorporate a batch estimator, provide precise information about the spacecraft state to be synchronized with scientific measurements. These tasks were conducted regularly to validate the results obtained by the MRO Navigation Tea...
The Mars Science Laboratory (MSL) spacecraft had ambitious navigation delivery and knowledge accurac...
Abstract—The Mars Reconnaissance Orbiter mission has as its primary objectives: advance our understa...
Determination of the spacecraft state has been traditional done using radiometric tracking data befo...
The Mars Reconnaissance Orbiter began science operations in November 2006, with a suite of seven ins...
This paper describes the orbit determination process, results and filter strategies used by the Mars...
The Mars Exploration Rover project consisted of two missions (MER-A: spirit rover and MER-B: opportu...
Carrying six science instruments and three engineering payloads, the Mars Reconnaissance Orbiter (MR...
The Mars Reconnaissance Orbiter (MRO) was launched from Cape Canaveral Air Force Station, Florida, U...
The MAVEN spacecraft will explore Mars' upper atmosphere. The primary science phase will last one (E...
Station. The heavyweight spacecraft will use a Lockheed-Martin Atlas V-401 launch vehicle. It will b...
Carrying six science instruments and three engineering payloads, the Mars Reconnaissance Orbiter (MR...
The Mars Reconnaissance Orbiter (MRO) was launched on August 12,2005 by an Atlas V 401 expendable la...
An orbit propagation software for the Mars orbiting spacecraft has been developed and verified in pr...
The Rotation and Interior Structure Experiment (RISE) on the InSight lander and the LaRa experiment ...
The Mars Reconnaissance Orbiter mission has as its primary objectives: advance our understanding of ...
The Mars Science Laboratory (MSL) spacecraft had ambitious navigation delivery and knowledge accurac...
Abstract—The Mars Reconnaissance Orbiter mission has as its primary objectives: advance our understa...
Determination of the spacecraft state has been traditional done using radiometric tracking data befo...
The Mars Reconnaissance Orbiter began science operations in November 2006, with a suite of seven ins...
This paper describes the orbit determination process, results and filter strategies used by the Mars...
The Mars Exploration Rover project consisted of two missions (MER-A: spirit rover and MER-B: opportu...
Carrying six science instruments and three engineering payloads, the Mars Reconnaissance Orbiter (MR...
The Mars Reconnaissance Orbiter (MRO) was launched from Cape Canaveral Air Force Station, Florida, U...
The MAVEN spacecraft will explore Mars' upper atmosphere. The primary science phase will last one (E...
Station. The heavyweight spacecraft will use a Lockheed-Martin Atlas V-401 launch vehicle. It will b...
Carrying six science instruments and three engineering payloads, the Mars Reconnaissance Orbiter (MR...
The Mars Reconnaissance Orbiter (MRO) was launched on August 12,2005 by an Atlas V 401 expendable la...
An orbit propagation software for the Mars orbiting spacecraft has been developed and verified in pr...
The Rotation and Interior Structure Experiment (RISE) on the InSight lander and the LaRa experiment ...
The Mars Reconnaissance Orbiter mission has as its primary objectives: advance our understanding of ...
The Mars Science Laboratory (MSL) spacecraft had ambitious navigation delivery and knowledge accurac...
Abstract—The Mars Reconnaissance Orbiter mission has as its primary objectives: advance our understa...
Determination of the spacecraft state has been traditional done using radiometric tracking data befo...