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[American Institute of Aeronautics and Astronautics Guidance and Control Conference - Cambridge,MA,U.S.A. (12 August 1963 - 14 August 1963)] Guidance and Control Conference - BANK ANGLE CONTROL SYSTEM FOR A SPINNING SATELLITE; APPENDIX A - RESPONSE OF SYMMETRICAL SPINNING VEHICLE TO TORQUE PULSES NORMAL TO SPINAXIS; APPENDIX B - STEADY-STATE EQUATIONS OF MOTION; APPENDIX C - DETERMINATION OF TOTAL NUMBER OF CORRECTIONS

✍ Scribed by PATAPOFF, H.

Book ID: 121019075
Publisher: American Institute of Aeronautics and Astronautics
Year: 1963
Weight: 493 KB
Category: Article
DOI: 10.2514/6.1963-339

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