NASA/SP-8036, Effects Of Structural Flexibility On Launch Vehicle Control Systems, NASA SPACE VEHICLE DESIGN CRITERIA (Guidance and Control), NASA (Washington, DC, United States), Massachusetts Inst. of Tech. (Cambridge, MA, United States), February,1970, pp. 51, Format(s): PDF 2953k |
Structural flexibility effects on launch vehicle control systems and design criteria.
| Keywords: | space vehicles, dynamic structural analysis, flexibility, launch vehicles, spacecraft control, systems engineering, deformation, environments, feedback control, mathematical models |
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| CASI Document ID Number: | 70N39774 |
| Subjects: | Astronautics: Spacecraft Design, Testing And Performance: Spacecraft Attitude Control And Stabilization |
| ID Code: | 72 |
| Deposited On: | 15 May 2002 |