NASA CR-2357 Feasilibility Study of an SSPS

FIGURE 28a. - VARIATION OF THE 1st ANTI-SYMMETRIC PITCH MODE FREQUENCY WITH RATE FEEDBACK GAIN FIGURE 28b. - VARIATION OF THE 1st ANTI-SYMMETRIC PITCH MODE FREQUENCY WITH RATE FEEDBACK GAIN

RkJQdWJsaXNoZXIy MTU5NjU0Mg==