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Dynamic
Concepts, Inc. personnel provided support to Sverdrup Technology
and Marshall Space Flight Center (MSFC) in performing a
6-DOF controllability analysis of an in-line Crew Experiment
Vehicle (CEV) Launch Vehicle concept. The launch vehicle
consisted of a 4-segment RSRM for first stage and a bi-propellant
single engine on second stage. Dynamic Concepts, Inc. performed
the following tasks:
-
Flex Body Bending Mode Analysis
- Launch
Vehicle 6-DOF Modeling
- POST
Trajectory Matching
- Open
Loop and Closed Loop Guidance
- SRB
Actuator Modeling (Freq Domain)
- Attitude
Control System Design with Gain Scheduling
- Flex
Body Filtering Design
- 6-DOF
Controllability Analysis using KSC 336 Winds
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