SHERPA (Strap-on High-altitude Entry Reconnaissance and Precision Aeromaneuver system) is a concept for low-cost-high-accuracy Martian reentry guidance for small scout-class missions with a capsule diameter of approximately 1 meter. This system uses moving masses to change the center of gravity of the capsule in order to control the lift generated by the controlled imbalance. This project involved designing a small proof-of-concept demonstration system that can be used to test the concept through bench-top testing, hardware-in-the-loop testing, and eventually through a drop test from a helicopter. This project has focused on the Mechatronic design aspects of the system including the mechanical, electrical, computer, and low-level control of the concept demonstration system.
SHERPA Electromechanical Test Bed
2005-08-01
Conference paper
No indication
English
Sherpa reaches few peaks Road test Sherpa 350 dropside
Automotive engineering | 1984
|Engineering Index Backfile | 1954
|Engineering Index Backfile | 1953
|Engineering Index Backfile | 1953
|