The Continuous System Modeling Program (CSMP) is described with its uses, its limitations, and its application to the rudder/speedbrake (R/SB) subsystem. The space shuttle R/SB is analyzed using the CSMP. Areas of analysis emphasized include: step response, ramp response, and the delay time or deadspace observed in system response. Results are presented and discussed.
Space Shuttle Rudder/Speedbrake Subsystem Analysis
1975
160 pages
Report
Keine Angabe
Englisch
Space shuttle rudder/speedbrake actuation subsystem
NTRS | 1985
|Space shuttle orbiter rudder/speedbrake actuation system
NTRS | 1981
|Space Shuttle aft Propulsion Subsystem
AIAA | 1981
|Space Shuttle Orbital Maneuver Subsystem
AIAA | 1975
|