Interplanetary spacecraft controllers using thrusters

Journal of Guidance, Control, and Dynamics

Volumn 21, Issue 4, 1998, Pages 542-550

  Hablani, Hari B ^a,b  

^a BOEING COMPANY   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; ORBITS; TORQUE; VECTORS; VELOCITY CONTROL;

PLANETARY ORBIT INSERTION; THRUSTER PULSES;

INTERPLANETARY SPACECRAFT;

EID: 0032123192     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4292     Document Type: Article

References (10)

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3. Hablani, H. B., "Interplanetary Spacecraft Controllers Using Thrusters," AIAA Guidance, Navigation, and Control Conference, AIAA, Reston, VA, 1997, pp. 1590-1612 (AIAA Paper 97-3754).
4. Wertz, J. R., Spacecraft Attitude Determination and Control, Reidel, Boston, MA, 1984, pp. 649-654.
5. Devey, W. J., Field, C. F., and Flook, L., "An Active Nutation Control System for Spin Stabilized Satellites," Proceedings of 6th IFAC Triennial World Congress (Boston/Cambridge, MA), 1975, pp. 14.1/1-10.
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8. Hablani, H. B., "Target Acquisition, Tracking, Spacecraft Attitude Control, and Vibration Suppression with IPFM Reaction Jet Controllers," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 4, 1994, pp. 831-839.
9. Cheng, R. K., and Pfeffer, I., "Terminal Guidance System for Soft Lunar Landing," Guidance and Control, edited by R. E. Roberson and J. S. Farrior, Vol. 8, Progress in Astronautics and Rocketry, Academic, New York, 1962, pp. 217-239.
10. Pfeffer, I., "Terminal Guidance for Soil Lunar Landing," Guidance and Control of Aerospace Vehicles, edited by C. T. Leondes, McGraw-Hill, New York, 1963, pp. 563-587.