BANK-TO- TURN MISSILES AND AUTOPILOT DESIGN | 東京工業大学附属図書館文献データベース

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BANK-TO- TURN MISSILES AND AUTOPILOT DESIGN

著者名:

KNILL RAF, T S , Flight Lieutenant ( LOUGHBOROUGH UNIVERSITY OF TECHNOLOGY AND ROYAL AIR FORCE COLLEGE CRANWELL )
Forsythe W , Dr phD MSc BSc
Lewis-Morris, M J , Flt Lt MSc BSc RAF

掲載資料名:

NASA Technical Reports

発行年:

1990

通号:

N93-23373

ペーパー番号:

N93-23373

出版情報:

National Aeronautics and Space Adminstration

言語:

英語

資料種別:

テクニカルペーパー

詳細

TDL書誌ID:

ZA00001429

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1 テクニカルペーパー A CONCEPTUAL DESIGN ANALYSIS OF AN AIR LAUNCHED ANTI-SATELLITE MISSILE SYSTEM Wishart, G K, BSc RAF, Render, P, Dr, Charnock, S, Squadron Leader, Lewis-Morris, M, Flight Lieutenant National Aeronautics and Space Adminstration	7 テクニカルペーパー Neural-adaptive nonlinear autopilot design for an agile anti-air missile McFarland, M.B., Calise, A.J. American Institute of Aeronautics and Astronautics
2 テクニカルペーパー Nonlinear Bank-to-Turn/Skid-to-Turn Missile Outer-Loop/Inner-Loop Autopilot Design with theta-D Technique Xin, M., Balakrishnan, S., Stansbery, D., Ohlmeyer, E. American Institute of Aeronautics and Astronautics	8 テクニカルペーパー A new approach to motion modeling and autopilot design of skid-to-turn missiles Song, Chanho, Kim, Yoon Sik American Institute of Aeronautics and Astronautics
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4 テクニカルペーパー An Overview of Flight Test Results for a Formation Flight Autopilot Hanson, C., Ryan, J., Allen, M., Jacobson, S. American Institute of Aeronautics and Astronautics	10 テクニカルペーパー HSCT configuration design using response surface approximations of supersonic euler aerodynamics Knill, D.L., Giunta, A.A., Baker, C.A., Grossman, B., Mason, W.H., Haftka, R.T., Watson, L.T. American Institute of Aeronautics and Astronautics
5 テクニカルペーパー Getting the full benefits of CFD in conceptual design Mason, W.H., Knill, D.L., Giunta, A.A., Grossman, B., Watson, L.T., Haftka, R.T. American Institute of Aeronautics and Astronautics	11 テクニカルペーパー Nonlinear optimal control design of a missile autopilot McLain, Timothy W., Beard, Randal W. American Institute of Aeronautics and Astronautics
6 テクニカルペーパー Missile Autopilot Design Using a New Suboptimal Nonlinear Control Method. Xin, M., Balakrishnan, S.N. American Institute of Aeronautics and Astronautics	12 テクニカルペーパー Predictive Estimation and Control Based Missile Autopilot Design Talole, S., Upreti, V., Phadke, S. American Institute of Aeronautics and Astronautics

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