DESIGN VERIFICATION AND FABRICATION OF ACTIVE CONTROL SYSTEMS FOR THE DAST ARW-2 HIGH ASPECT RATIO WING, PART 2 - APPENDICES

摘要

A study is presented in Appendix B that compares servoactuator bench test results to analysis and investigates various factors that affect actuator performance and stability. Appendix C contains data which summarizes the airplane stability and performance with the final flutter suppression system. The data contained in Appendix D shows stability and performance sensitivity to variation in the dynamics and location of the control system components. Appendix E contains data that shows the relative gain and phase stability margins of each individual ACS and AFCS feedback loop and the compatibility of the combined loops.