Rensselaer's roving vehicle for Mars
Single module unmanned Mars roving vehicle with flexible metal toroidal hoop-spoked wheels, discussing remote controlled scale model design for simulation on earth
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Single module unmanned Mars roving vehicle with flexible metal toroidal hoop-spoked wheels, discussing remote controlled scale model design for simulation on earth
A design for a Mars Roving Vehicle is presented in a three dimensional model considering three degrees of freedom. In addition, the physical characteristics of the 0.4 scale RPI-MRV are presented along with the basic dynamic responses.
Man-machine system for extraterrestrial surface roving vehicles
Reliability of Surveyor lunar roving vehicle design - mathematical models, failure modes, and predictions
Surveyor Lunar Roving Vehicle /SLRV/ mission in support of Apollo LEM program
Dead reckoning navigation system for manned lunar roving vehicle
Optimal traction drive system design for lunar roving vehicle, considering weight, energy consumption, operational flexibility, power supply, motor and power train
Routing algorithm for computer controlled unmanned autonomous roving vehicle on Martian surface
Dual mode algorithm for routing unmanned autonomous roving vehicle around obstacles on planets, using dynamic programming and terrain information
Mobility and structural analyses of bellows concept for lunar roving vehicle
Auxiliary power systems and life support and cabin environmental control systems for lunar roving vehicle
Visual simulation facility for evaluation of lunar surface roving vehicles
Computer system functional requirements for autonomous Martian surface roving vehicle, emphasizing vehicle motion control system
Optimum design considerations of traction drive for lunar roving vehicle
The qualification model of the lunar roving vehicle (LRV) was tested in the Spacecraft Magnetic Test Facility (SMTF) at the GSFC Magnetic Test Site. Magnetic field measurements were made, both with the vehicle in its as received state and also subsequent to final deperm treatment. These measurements, together with information supplied to GSFC regarding the magnetic moment of the astronaut's extravehicular mobility units (EMU's) were used to calculate 0.5 nanotesla (gamma) contours around the LRV. The results are tabulated. Magnetic field measurements were also made with various items of LRV equipment operational. No significant changes were noted, except during operation of the vehicle wheels.
The complete electronics packaging which controls the Mars roving vehicle is described in order to provide a broad overview of the systems that are part of that package. Some software debugging tools are also discussed. Particular emphasis is given to those systems that are controlled by the microprocessor. These include the laser mast, the telemetry system, the command link prime interface board, and the prime software.
System functional requirements and configurations for roving vehicle missions on Moon and Mars - motion control
Roving vehicle payload for Surveyor lunar soft landing spacecraft