Developments in the field of automatic guidance and control of rockets

Journal of Guidance, Control, and Dynamics

Volumn 4, Issue 3, 1981, Pages 225-239

  Haeussermann, Walter ^a  

^a HONEYWELL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 85003360417     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.19735     Document Type: Article

References (15)

1. Farrior, J.S., “Inertial Guidance, Its Evolution and Future Potential,” From Peenemuende to Outer Space, NASA Marshall Space Flight Center, March 23, 1962.
2. Mueller, F.K., “A History of Inertial Guidance,” Army Ballistic Missile Agency, Redstone Arsenal, Ala., 1960.
3. Mueller, O., “The Control System of the V-2, History of German Guided Missile Development,” edited by Th. Benecke and A.W. Quick, AGARD Seminar, Munich, Federal Republic of Germany, 1956.
4. Hoelzer, H., “Guidance and Control Symposium,” AAS Vol. 43, Science and Technology, 1976, pp. 301-316.
5. Haeussermann, W., “On the Evolution of Rocket Navigation, Guidance and Control Systems,” AAS Vol. 43, Science and Technology, 1976, pp. 258-269.
6. Haeussermann, W. and Duncan, R.C., “Status of Guidance and Control Methods, Instrumentation, and Techniques as Applied in the Apollo Project,” Lecture Series on Orbit Optimization and Advanced Guidance Instrumentation, AGARD, Duesseldorf, Federal Republic of Germany, Oct. 1964.
7. Haeussermann, W., “The Delta Minimum Inertial Guidance Scheme,” 13th Annual Meeting of the American Rocket Society, New York, N.Y., Nov. 1958
8. Pickering, W.H., “History of the Cluster System,” From Peenemuende to Outer Space, NASA Marshall Space Flight Center, March 23, 1962.
9. Hosenthien, H.H. and Boehm, J., “Flight Simulation of Rockets and Spacecraft,” From Peenemuende to Outer Space, NASA Marshall Space Flight Center, March 23, 1962.
10. Haeussermann, W., “Spatial Attitude Control of a Spinning Cluster,” ARS Journal, Vol. 29, Jan. 1959, pp. 56-58.
11. Haeussermann, W., “Saturn Launch Vehicle’s Navigation, Guidance and Control System,” Automatica, Vol. 7, Sept. 1971, pp. 537-556.
12. Chandler, D.C., Horn, H.J., and Martin, D.T., “An Iterative Guidance Scheme and Its Application to Lunar Landing,” NASA Marshal Space Flight Center, MTP-Aero, 63-11, Feb. 6, 1963.
13. Faget, M.A., “The Evolution of Flight Control of the Apollo Mission,” AAS Vol. 45, Science and Technology, 1977, pp. 324-330.
14. Haeussermann, W., “Stability Areas of Missile Control Systems,” Jet Propulsion, Vol. 27, July 1957, pp. 787-795.
15. Asner, B. and Seltzer, S.M., “Parameter Plane Analysis for Large Flexible Spacecraft,” Journal of Guidance and Control, Vol. 4, May-June 1981, pp. 284-290 (this issue).