A remote control system for testing on maneuverable parachutes was designed. The feasibility of trajectory control of heavy load parachutes by a remote system was analyzed. The feasibility of automatic guidance of payloads accompanied by a parachutist was examined. A parachute wing and a parachute model were constructed. Analysis and test results enabled the characteristics of an operational system to be derived.
Teleguidage des Charges Sous Parachutes Manoeuvrables (Remote Guidance of Payloads under Maneuverable Parachutes)
1988
173 pages
Report
No indication
English
SLUB | 1951
|Engineering Index Backfile | 1921
|Engineering Index Backfile | 1929
|NTRS | 1925
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