Preliminary Gemini 4 Crew Debriefing, Part I, 1965
NASA-UAP-D016 · page 276 of 340
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268 other hand, it didn't seem to make the space craft roll either. Then I turned that ring off and went over and ddd it on the other ring. Identically the same thing happened. I thought I might have trouble with the roll -gyro . I turmid the roll gyro to SECONDARY. That didn 't seem to make any difference. We went back to PRIMARY . I remember commenting at that time that the RCS was a lot looser in control than the OAMS. It seemed to me that the OAMS held the spacecraft attitude better. It seemed like it controlled to a rate deadband that was smaller than the RCS deadband. I don't know why you're using the same gyros and the same electronics. The only thing that could be different would be the attitude drivers on the RCS might be activiating slower than they are in the OAMS. It seemed like the rates were such a--seems like there must be a lag in the whole system. It seemed like the deadband in the RCS was twice what it was in the OAMS . It operated properly. There's so much difference between looking at that ball on firing retros ~N-FIE>ENl~L