7.6 References

1. WEYMEYER, W.K, and SPORING, R.W.: 'An industry survey on aeroelastic control system instabilities in aerospace vehicles.' IAS paper. 62-47, January 1962

2. HOFMANN, L.G, and KEZER, A.: 'Simplified analysis of flexible booster FCS.' MITE-1210, June 1962

3. 'Notes on some problems of high speed aircraft programmes.' Royal Aircraft Establishment TMIAP-649, March 1957

4. FELT, L.R., HUTTSELL, L.J., NOLL, T.E, and COOLEY, D.E.: 'Aeroservoelastic encounters', J. Aircr., July 1979, 16, (7), article 78-1289

5. NORRIS, G.: 'Amraam block placed on Lockheed F-16s. 'Flight International, 20 October 1993

6. KEHOE, M.W., LAURIE, E.J., and BJARKE, L.J.: 'An inflight interaction of the X-29A canard and FCS.' AIAA-90-1240-CP, 1990

7. THOMPSON, M.O.: 'At The Edge of Space-The X-15 Flight Programme.' Airlife, 1990

8. EVANS, G.J., and BEELE, B.J.: 'Auto aeroelastic mode coupling, a comparison of predicted and actual characteristics.' AGARD FMP S&C, September 1968

9. TAYLOR, R., PRATT, R.W. and CALDWELL, B.D.: 'The effect of actuator non-linearities on ASE.' J. Guid. Contr. Dynam, March 1996, 19, (2)

10. FCS-'design installation and test of piloted aircraft, general specification for.' MIL-F-9490D

11. TRETTER S.A.: 'Discrete Time Signal Processing.' (John Wiley and Sons, 1976)

12. TAYLOR, R., PRATT, R.W., and CALDWELL, B.D.: 'The effects of sampled signals on the FCS of an agile combat aircraft with a flexible structure.' Proc. American Control conference, Seattle, 1, June 1995, pp. 505-509. Also, Trans. Inst. Meas. Control, March 1996., 18, 3 pp. 160-164

13. NANSON, K.M., and RAMSEY, R.B.: 'The development and use of inflight analysis at B. Ae. Warton.'...