Spacecraft dynamics and control: A practical engineering approach

Spacecraft Dynamics and Control: A Practical Engineering Approach

Volumn , Issue , 2014, Pages 1-409

  Sidi, Marcel J ^a  

^a TEL AVIV UNIVERSITY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

DYNAMICS; LIQUID SLOSHING; ORBITS; SPACECRAFT; STABILIZATION; STRUCTURAL DYNAMICS;

ATTITUDE STABILIZATION; ENGINEERING PROBLEMS; GRAVITY-GRADIENT STABILIZATION; ONBOARD CONTROL SYSTEMS; PRACTICAL ENGINEERING; SCIENTIFIC RESEARCHES; SPACECRAFT DYNAMICS; SPIN STABILIZATION;

SPIN DYNAMICS;

EID: 84953375811     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1017/CBO9780511815652     Document Type: Book

References (203)

1. Bittner, H., Fisher, H., Miltenberger, K., Roche, Z. C., Scheit, A., Surauer, M., and Vieler, H. (1987), "The Attitude and Orbit Control Subsystem of the DFS Koper-nikus," Automatic Control World Congress, IFAC (27-31 July, Munich). Oxford: Pergamon.
2. Bittner, H., Fisher, H., Froeliger, J., Miltenberger, K., Popp, H., Porte, F., and Surauer, M. (1989), "The Attitude and Orbit Control Subsystem of the EUTELSAT II Spacecraft," 11th IFAC Symposium on Automatic Control in Space (17-21 July, Tsu-kuba, Japan).
3. Dougherty, H., Scott, E., and Rodden, J. (1968), "Analysis and Design of WHECON-An Attitude Control Concept," Paper no. 68-461, AIAA 2nd Communications Satellite System Conference (8-10 April, San Francisco). New York: AIAA.
4. Agrawal, B. N. (1986), Design of Geosynchronous Spacecraft. Englewood Cliffs, NJ: Prentice-Hall.
5. Alby, F. (1983), "Les Perturbations de l’Orbite Geostationaire," in The Motion of the Satellite, Lectures and Exercises on Space Mechanics. Toulouse, France: Cepadues-Editions, pp. 569-611.
6. Balmino, G. (1980), "Le Mouvement Elliptique Perturbe," in LeMouvement du Vehicule Spatial en Orbite. Toulouse, France: Centre National d’Etudes Spatiales, pp.59-84.
7. Bate, R. R., Mueller, D. D., and White, J. E. (1971), Fundamentals of Astrodynamics. New York: Dover.
8. Battin, R. H. (1990), An Introduction to the Mathematics and Methods of Astrodynamics. Washington, DC: AIAA.
9. Bernard, J. (1983), "Mouvement Keplerien et Perturbe," in The Motion of the Satellite Lectures and Exercises on Space Mechanics. Toulouse, France: Cepadues-Editions, pp. 25-86.
10. Borderies, N. (1980), "Les Perturbation d’Orbites: les Effets," in Le Mouvement du Vehicule Spatial en Orbite. Toulouse, France: Centre National d’Etudes Spatiales, pp. 131-51.
11. Breakwell, J., and Roberson, R. (1970), "Orbital and Attitude Dynamics," Lecture notes, Stanford University.
12. Campan, G. (1983), "Les Perturbations d’Orbite," in The Motion of the Satellite, Lectures and Exercises on Space Mechanics. Toulouse, France: Cepadues-Editions, pp. 129-57.
13. Chobotov, V. A. (1991), Orbital Mechanics. Washington, DC: AIAA.
14. Deutsch, R. (1963), Orbital Dynamics of Space Vehicles. Englewood Cliffs, NJ: Prentice-Hall.
15. Escobal, P. R. (1965), Methods of Orbit Determination. Malabar, FL: Krieger.
16. Kaplan, M. H. (1976), Modern Spacecraft Dynamics and Control. New York: Wiley.
17. Legendre, P. (1980), "Mantien a Poste des Satellites Geostationaires: Strategic des Corrections d’Orbite," in Le Mouvement du Vehicule Spatial en Orbite. Toulouse, France: Centre National d’Etudes Spatiales, pp. 583-609.
18. Pocha, J. J. (1987), An Introduction to Mission Design for Geostationary Satellites. Dordrecht: Reidel.
19. Pritchard, L. W., and Sciulli, A. J. (1986), Satellite Communication Systems Engineering. Englewood Cliffs, NJ: Prentice-Hall.
20. Soop, E. M. (1983), Introduction to Geostationary Orbits. Paris: European Space Agency.
21. Thomson, W. T. (1986), Introduction to Space Dynamics. New York: Dover.
22. Wertz, J. R. (1978), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.
23. Agrawal, B. N. (1986), Design of Geosynchronous Spacecraft. Englewood Cliffs, NJ: Prentice-Hall.
24. Alby, F. (1983), "Les Perturbations de POrbite Geostationaire," in The Motion of the Satellite Lectures and Exercises on Space Mechanics. Toulouse, France: Cepadues-Editions, pp. 569-611.
25. Belon, B. (1983), "Stratégic de Maintien a Poste des Satellites Géostationaires," in The Motion of the Satellite Lectures and Exercises on Space Mechanics. Toulouse, France: Cépadués-Éditions, pp. 613-42.
26. Deutsch, R. (1963), Orbital Dynamics of Space Vehicles. Englewood Cliffs, NJ: Prentice-Hall.
27. Duret, F., and Frouard, J. P. (1980), Conception Générate des Systémes Spatiaux, Conception des Fusées Porteuses. Toulouse, France: Ecole National de l’Aeronautique et de TEspace.
28. Gantous, D. J. (1986), "Eccentricity Control Strategy for Geosynchronous Communication Satellites," in Space Dynamics for Geostationary Satellites. Toulouse, France: Cépadues-Éditions, pp. 693-704.
29. Kaplan, M. H. (1976), Modern Spacecraft Dynamics and Control. New York: Wiley.
30. Legendre, P. (1980), "Maintien a Poste des Satellites Géostationaires: Stratégie des Corrections d’Or bite," in Le Mouvement du Véhicule Spatial en Orbite. Toulouse, France: Centre National d’Études Spatiales, pp. 583-609.
31. Pocha, J. J. (1987), An Introduction to Mission Design for Geostationary Satellites. Dor-drecht: Reidel.
32. Pritchard, W., and Sciulli, J. (1986), Satellite Communication Systems Engineering. Englewood Cliffs, NJ: Prentice-Hall.
33. Prussing, J. (1991), "Simple Proof of the Global Optimality of the Hohmann Transfer," Journal of Guidance Control and Dynamics 15(4): 1037-8.
34. Redding, D. C. (1984), "Highly Efficient, Very-Low-Thrust Transfer to Geosynchronous Orbit: Exact and Approximate Solutions," Journal of Guidance Control and Dynamics 7(2): 141-7.
35. Robbins, H. M. (1966), "An Analytical Study of the Impulsive Approximation,1" AIAA Journal 4:1417-23.
36. Robert, J. M., and Foliard, J. (1980), "Satellite Geostationaire," in Le Mouvement du Vehicule Spatial en Orbite. Toulouse, France: Centre National d’Etudes Spatiales, pp. 505-57.
37. Slavinskas, D., Dabbaghi, H., Bendent, W., and Johnson, G. (1988), "Efficient Inclination Control for Geostationary Satellites," Journal of Guidance Control and Dynamics 11(6): 584-9.
38. Soop, M. E. (1983), Introduction to Geostationary Orbits. Paris: European Space Agency.
39. Soop, M. E., and Morley, T. (1989), "A Portable Program Package for Geostationary Orbit Control (PEPSOC)," Spacecraft Trajectory Branch, Orbit Attitude Division, European Space Operations Center, Darmstadt, Germany.
40. Bracewell, R. N., and Garriott, O. K. (1958), "Rotation of Artificial Earth Satellites," Nature 82: 760-2.
41. Goldstein, H. (1964), Classical Mechanics. Reading, MA: Addison-Wesley.
42. Greensite, A. (1970), Analysis and Design of Space Vehicles Flight Control Systems. New York: Spartan Books.
43. Hildebrand, F. (1968), Methods of Applied Mathematics. New Delhi: Prentice-Hall.
44. Kaplan, M. (1976), Modern Spacecraft Dynamics and Control. New York: Wiley.
45. Kaplan, W. (1953), Advanced Calculus. Reading, MA: Addison-Wesley.
46. Thomson, W. T. (1986), Introduction to Space Dynamics. New York: Dover.
47. Wertz, J. R. (1978), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.
48. Bryson, A. (1983), "Stabilization and Control of Spacecraft," Microfiche supplement to the Proceedings of the Annual AAS Rocky Mountain Guidance and Control Conference (5-9 February, Keystone, CO). San Diego, CA: American Astronautical Society.
49. Clopp, W., and Osborn, L. (1987), "Satellite Bus Design for the Multiple Satellite System," AIAA/DARPA Meeting on Lightweight Satellite Systems (4-6 August, Monterey, CA). Washington, DC: AIAA, pp. 105-15.
50. Fleeter, R., and Warner, R. (1989), "Guidance and Control of Miniature Satellites," Automatic Control in Aerospace, IFAC (Tsukuba, Japan). Oxford, UK: Pergamon, pp. 243-8.
51. Hughes, P. C. (1988), Spacecraft Attitude Dynamics. New York: Wiley.
52. Kaplan, M. (1976), Modern Spacecraft Dynamics and Control. New York: Wiley.
53. Martel, F., Pal, P., and Psiaki, M. (1988), "Active Magnetic Control System for Gravity Gradient Stabilized Spacecraft," Second Annual AIAA/USU Conference on Small Satellites (26-28 September, Logan, UT). Washington, DC: AIAA.
54. Runavot, J. J. (1980), "Le Systeme de Commande d’Attitude et d’Orbite: Généralites et Definition du Systéme," in Le Mouvement du Véhicule Spatial en Orbite. Toulouse, France: Centre National d’Études Spatiales, pp. 909-28.
55. William, H. C., and Osborn, L. (1987), "Satellite Bus and Design for the Multiple Satellite System," AIAA/DARPA Meeting on Lightweight Satellite Systems (4-6 August, Monterey, CA). Washington, DC: AIAA.
56. Agrawal, B. N. (1986), Design of Geosynchronous Spacecraft. Englewood Cliffs, NJ: Prentice-Hall.
57. Bryson, A. (1983), "Stabilization and Control of Spacecraft," Microfiche supplement to the Proceedings of the Annual AAS Rocky Mountain Guidance and Control Conference (5-9 February, Keystone, CO). San Diego, CA: American Astronautical Society.
58. Devey, W., Field, C., and Flook, L. (1977), "An Active Nutation Control System for Spin Stabilized Satellites," Automatica 13:161-72.
59. Fagg, A., and MacLauchlan, J. (1981), "Operational Experience on OTS-2," Journal of Guidance and Control 4(5): 551-7.
60. Fox, S. (1986), "Attitude Control Subsystem Performance of the RCA Series 3000 Satellite," Paper no. 86-0614-CP, AIAA 11th Communications Satellite System Conference (17-20 March, San Diego). New York: AIAA.
61. Garg, S. C., Farimoto, N., and Vanyo, Y. P. (1986), "Spacecraft Nutational Instability. Prediction by Energy Dissipation Measurements," Journal of Guidance Control and Dynamics 9(3): 357-62.
62. Grasshoff, L. H. (1968), "An Onboard, Closed-Loop Nutation Control System for a Spin-Stabilized Spacecraft," Journal of Spacecraft and Rockets 5(5): 530-5.
63. Grumer, M., Komem, Y., Kronenfeld, J., Kubitski, O., Lorber, V., and Shyldkrot, H. (1992), "OFEQ-2: Orbit, Attitude and Flight Evaluation," 32nd Israel Annual Conference on Aviation and Astronautics (18-20 February, Tel Aviv). Tel Aviv: Kenes, pp. 266-78.
64. Iorillo, A. J. (1965), "Nutation Damping Dynamics of Axisymmetric Rotor Stabilized Satellites," ASME Winter Meeting (November, Chicago). New York: ASME.
65. Likins, P. (1967), "Attitude Stability Criteria for Dual-Spin Spacecraft," Journal of Spacecraft and Rockets 4(12): 1638-43.
66. Webster, E. A. (1985), "Active Nutation Control for Spinning Solid Motor Upper Stages," Paper no. 85-1382, 21st Joint Propulsion Conference, AIAA/SAE/ASME (8-10 July, Monterey, CA).
67. Azor, R. (1993), "Momentum Management and Torque Distribution in a Satellite with Reaction Wheels," Israel Annual Conference on Aviation and Astronautics (24-25 February, Tel Aviv). Tel Aviv: Kenes, pp. 339-47.
68. Bikdash, M., Cliff, E., and Nayfeh, A. (1993), "Saturating and Time Optimal Feedback Controls," Journal of Guidance, Control, and Dynamics 16(3): 541-8.
69. Bilimora, K., and Wie, B. (1993), "Time-Optimal Three-Axis Reorientation of a Rigid Spacecraft," Journal of Guidance, Control, and Dynamics 16(3): 446-60.
70. Bollner, M. (1991), "On-board Control System Performance of the Rosat Spacecraft," Acta Astronautica 25(8/9): 487-95.
71. Boorg, P. (1982), "Validation for Spot Attitude Control System Development," IFAC Automatic Control System Development. Noordwijk, Netherlands, pp. 67-73.
72. Bosgra, J. A., and Prins, M. J. (1982), "Testing and Investigation of Reaction Wheels," IFAC Automatic Control in Space. Noordwijk, Netherlands, pp. 449-58.
73. Bosgra, J. A., and Smilde, H. (1982), "Experimental and Systems Study of Reaction Wheels. Part I: Measurement and Statistical Analysis of Forces and Torque Irregularities," National Aerospace Laboratory, NLR, Netherlands.
74. Bryson, A., and Ho, Y. (1969), Applied Optimal Control. Waltham, MA: Blaisdel.
75. D’Azzo, J. J., and Houpis, C. H. (1988), Linear Control System Analysis and Design, Conventional and Modern. New York: McGraw-Hill.
76. Dorf, C. R. (1989), Modern Control Systems. 5th ed. Reading, MA: Addison-Wesley.
77. Dougherty, H., Rodoni, C., Tompetrini, K., and Nakashima, A. (1982), "Space Telescope Control," IFAC Automatic Control in Space. Oxford, UK: Pergamon, pp. 15-24.
78. Elgerd, O. (1967), Control System Theory. New York: McGraw-Hill.
79. Fleming, A. W., and Ramos, A. (1979), "Precision Three-Axis Attitude Control via Skewed Reaction Wheel Momentum Management," Paper no. 79-1719, AIAA Guidance and Control (6-8 August, Boulder, CO). New York: AIAA, pp. 177-90.
80. Glaese, J. R., Kennel, H. F., Nurre, G. S., Seltzer, S. M., and Shelton, H. L. (1976), "Low-Cost Space Telescope Pointing Control System," Journal of Spacecraft and Rockets 13(7): 400-5.
81. James, H. M., Nichols, N. B., and Phillips, R. S. (1955), Theory of Servomechanisms (MIT Radiation Laboratory Series, vol. 25). New York: McGraw-Hill.
82. Junkins, J. L., and Turner, J. D. (1986), Optimal Spacecraft Rotational Maneuvers. Amsterdam: Elsevier.
83. Kaplan, M. (1976), Modern Spacecraft Dynamics and Control. New York: Wiley.
84. Lebsock, K. (1982), "Magnetic Desaturation of a Momentum Bias System," AIAA/AAS Astrodynamics Conference (9-11 August, San Diego). New York: AIAA.
85. McElvain, R. J. (1962), "Satellite Angular Momentum Removal Utilizing the Earth’s Magnetic Field," Space Systems Division, Hughes Aircraft Co., El Segundo, CA.
86. Oh, H. S., and Valadi, S. R. (1991), "Feedback Control and Steering Laws for Spacecraft Using Single Gimbal Control Moment Gyros," Journal of the Astronautical Sci-ences 39(2): 183-203.
87. Pierre, A. D. (1986), Optimization Theory with Applications. New York: Dover.
88. Pircher, M. (1989), "Spot 1 Spacecraft in Orbit Performance," IFAC Automatic Control in Space. Noordwijk, Netherlands.
89. Schletz, B. (1982), "Use of Quaternion in Shuttle Guidance," Paper no. 82-1557, AIAA Conference on Navigation and Control (9-11 August, San Diego). New York: AIAA, pp. 753-60.
90. Solodovnikov, V. V. (1960), Introduction to the Statistical Dynamics of Automatic Control Systems. New York: Dover.
91. Stickler, A. C., and Alfriend, K. (1976), "Elementary Magnetic Attitude Control System," Journal of Spacecraft and Rockets 13(5): 282-7.
92. Wertz, J. R. (1986), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.
93. Wie, B., Weiss, H., and Arapostathis, A. (1989), "Quaternion Feedback Regulator for Spacecraft Eigenaxis Rotations," Journal of Guidance, Control, and Dynamics 12(3): 375-80.
94. Agrawal, B. N. (1986), Design of Geosynchronous Spacecraft. Englewood Cliffs, NJ: Prentice-Hall.
95. Azor, R. (1992), "Solar Attitude Control Including Active Denutation Damping in a Fixed Momentum Wheel Satellite," AIAA Guidance Navigation and Control Conference (10-12 August, Hilton Head Island, SC). Washington, DC: AIAA, pp. 226-35.
96. Azor, R. (1995), "Roll/Yaw Attitude Control and Denutation by Thrusters," Israel Annual Conference on Aviation and Astronautics (February, Tel Aviv). Tel Aviv: Kenes, pp.86-94.
97. Benoit, A., and Bailly, M. (1987), "In-Orbit Experience Gained with the European OTS/ECS/TELECOM 1 Series of Spacecraft" (AAS 87-054), Proceedings of the Annual Rocky Mountain Guidance and Control Conference (31 January-4 February 1987, Keystone, CO). San Diego, CA: American Astronautical Society, pp.525-42.
98. Bingham, N., Craig, A., and Flook, L. (1984), "Evolution of European Telecommunication Satellite Pointing Performance," Paper no. 84-0725, AIAA, New York.
99. Bittner, H., Bruderle, E., Roche, Ch., and Schmidts, W. (1977), "The Attitude Determination and Control Subsystem of the Intelsat V Spacecraft" (ESA SP-12), Proceedings of AOCS Conference (3-6 October, Noordwijk, Netherlands). Paris: European Space Agency.
100. Bryson, A. (1983), "Stabilization and Control of Spacecraft," Microfiche supplement to the Proceedings of the Annual A AS Rocky Mountain Guidance and Control Conference (5-9 February, Keystone, CO). San Diego, CA: American Astronautical Society.
101. Devey, W. J., Field, C. F., and Flook, L. (1977), "An Active Nutation Control System for Spin Stabilized Satellites "Automatica 13:161-72.
102. Dougherty, H. J., Lebsock, K. L., and Rodden, J. J. (1971), "Attitude Stabilization of Synchronous Communications Satellite Employing Narrow-Beam Antennas," Journal of Spacecraft and Rockets 8: 834-41.
103. Dougherty, H. J., Scott, E. D., and Rodden, J. J. (1968), "Analysis and Design of WHECON-An Attitude Control Concept," Paper no. 68-461, AIAA 2nd Communications Satellite Systems Conference (8-10 April, San Francisco).
104. Duhamel, T., and Benoit, A. (1991), "New AOCS Concepts for ARTEMIS and DRS,". Space Guidance, Navigation and Control Systems (Proceedings of the First EAS International Conference, ESTEC, 4-7 June, Noordwijk, Netherlands). Paris: European Space Agency, pp. 33-9.
105. Forward, R. L. (1990), "Grey Solar Sails," Journal of the Astronautical Sciences 38(2): 161-85.
106. Fox, S. (1986), "Attitude Control Subsystem Performance of the RCA Series 3000 Satellite," Paper no. 86-0614-CP, AIAA 11th Communications Satellite System Conference (17-20 March, San Diego, CA).
107. Georgevic, R. M. (1973), "The Solar Radiation Pressure Force and Torques Model," Journal of the Astronautical Sciences 20(5): 257-74.
108. Iwens, R. P., Fleming, A. W., and Spector, V. A. (1974), "Precision Attitude Control with a Single Body-Fixed Momentum Wheel," Paper no. 74-894, AIAA Mechanics and Control of Flight Conference (5-9 August, Anaheim, CA).
109. Lebsock, K. L. (1980), "High Pointing Accuracy with a Momentum Bias Attitude Control System," Journal of Guidance and Control 3(3): 195-202.
110. Lebsock, K. L. (1982), "Magnetic Desaturation of a Momentum Bias System," Paper no. 82-1468, AIAA/AAS Astrodynamics Conference (9-11 August, San Diego, CA).
111. Lievre, J. (1985), "Solar Sailing Attitude Control of Large Geostationary Satellite," IFAC Automatic Control in Space. Oxford, UK: Pergamon, pp. 29-33.
112. Maute, P., Blancke, B., Jahier, J., and Alby, F. (1989), "Autonomous Geostationary Sta-tionkeeping System Optimization and Validation," Acta Automatica 20: 93-101.
113. Muhlfelder, L. (1984), "Attitude Control System Evolution of Body-Stabilized Communication Spacecraft," Paper no. 84-1839, AIAA Guidance and Control Conference (20-22 August, Seattle). Washington, DC: AIAA, pp. 55-62.
114. Phillips, K. (1973), "Active Nutation Damping Utilizing Spacecraft Mass Properties," IEEE Transactions on Aerospace and Electronic Systems 9(5): 688-93.
115. Renner, U. (1979), "Attitude Control by Solar Sailing-A Promising Experiment with OTS-2," ESA Journal 3(1): 35-40.
116. Schmidt, G. E. (1975), "The Application of Magnetic Attitude Control to a Momentum-Biased Synchronous Communication Satellite," Paper no. 75-1055, AIAA Guidance and Control Conference (20-22 August, Boston).
117. Schmidt, G. E., and Mulhfelder, L. (1981), "The Application of Magnetic Torquing to Spacecraft Attitude Control" (AAS 81-002), Proceedings of the Annual Rocky Mountain Guidance and Control Conference (31 January-4 February, Keystone, CO). San Diego, CA: American Astronautical Society.
118. Sidi, M. (1992a), "Attitude Stabilization of Bias-Momentum Satellites," Israel Annual. Conference on Aviation and Astronautics (18-20 February, Tel Aviv). Tel Aviv: Kenes, pp. 333-8.
119. Sidi, M. (1992b), "Reactive Thrust Cruise for a Geosynchronous Bias-Momentum Satellite with Active Denutation," 12th FAC Symposium in Aerospace Control (7-11 September, Ottobrunn, Germany). Oxford, UK: Pergamon, pp. 201-5.
120. Wertz, J. R. (1978), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.
121. Wie, B., Lehner, J., and Plescia, C. (1985), "Roll/Yaw Control of Flexible Spacecraft Using Skewed Bias Momentum Wheels," Journal of Guidance, Control and Dynamics 8(4): 447-51.
122. Bittner, H., Fisher, H., and Surauer, M. (1982), "Design of Reaction Jet Attitude Control Systems for Flexible Spacecraft," IFAC Automatic Control in Space. Noordwijk, Netherlands: IFAC, pp. 373-98.
123. Chan, N. (1982), Ford Aerospace and Communications Corporation Patent Application for "Digital PWPF Three-Axis Spacecraft Attitude Control," US(SN) 407-196, filed 11 August.
124. D’Azzo, J., and Houpis, C. (1988), Linear Control System Analysis and Design, Conventional and Modern. New York: McGraw-Hill.
125. Franklin, F., and Powell, J. (1980), Digital Control of Dynamic Systems. Reading, MA: Addison-Wesley.
126. Horowitz, I. (1963), Synthesis of Feedback Systems. New York: Academic Press.
127. Houpis, H., and Lamont, G. (1985), Digital Control Systems: Theory, Hardware, and Software. New York: McGraw-Hill.
128. Joice, M., and Clarke, K. (1961), Transistor Circuit Analysis. Reading, MA: Addison-Wesley.
129. Kuo, C. (1970), Discrete-Data Control Systems. Englewood Cliffs, NJ: Prentice-Hall.
130. Millman, J., and Taub, H. (1956), Pulse and Digital Circuits. New York: McGraw-Hill.
131. Saucedo, R., and Schiring, E. (1968), Introduction to Continuous and Digital Control Systems. New York: Macmillan.
132. Sidi, M. (1973), "Synthesis of Feedback Systems with Large Plant Ignorances for Prescribed Time-Domain Tolerances," Ph.D. dissertation, Weizman Institute of Science, Rehovot, Israel.
133. Sidi, M. (1977), "Synthesis of Sampled Feedback Systems for Prescribed Time Domain Tolerances," International Journal of Control 26(3): 445-61.
134. Sidi, M. (1980), "On Maximization of Gain-Bandwidth in Sampled Systems," International Journal of Control 32(6): 1099-1109.
135. Vaeth, J. (1965), "Compatibility of Impulse Modulation Techniques with Attitude Sensor Noise and Spacecraft Maneuvering," IEEE Transactions on Automatic Control 10: 67-76.
136. Wie, B., and Plescia, C. (1984), "Attitude Stabilization of Flexible Stationkeeping Maneuvers," Journal of Guidance Control and Dynamics 7(4): 430-6.
137. Abramson, H. (1961), "The Dynamic Behavior of Liquids in Moving Containers," NASA SP-106 (N67-15884), Scientific and Technical Information Division, National Aeronautics and Space Administration, Washington, DC.
138. Bode, H. W. (1945), Network Analysis and Feedback Amplifier Design. New York: Van Nostrand.
139. Bryson, A. (1983), "Stabilization and Control of Spacecraft," Microfiche supplement to the Proceedings of the Annual AAS Rocky Mountain Guidance and Control Conference (5-9 February, Keystone, CO). San Diego, CA: American Astronautical Society.
140. Peterson, D., Crawley, E., and Hansman, R. (1988), "Nonlinear Fluid Slosh Coupled to the Dynamics of a Spacecraft," A4/A4 Journal 27(9): 1230-40.
141. Pocha, J. (1986), "An Experimental Investigation of Spacecraft Sloshing," Paper no. 255. Proceedings of the Second International Symposium on Spacecraft Flight Dynamics (20-23 October, Darmstadt, Germany). Paris: European Space Agency.
142. Prins, J. (1983), "Trends in AOCS Testing," IFAC Workshop (August, Stanford, CA).
143. Sidi, M. (1976), "Feedback Synthesis with Plant Ignorance, Non-minimum-Phase, and Time-Domain Tolerances," Automatica 12: 265-71.
144. Sidi, M. (1980), "On Maximization of Gain-Bandwidth in Sampled Systems," International Journal of Control 32(6): 1099-1109.
145. Sidi, M., and Horowitz, I. (1973), "Synthesis of Feedback Systems with Large Plant Ignorance for Prescribed Time Domain Tolerances," Sensitivity Adaptivity and Optimality (Proceedings of the Third IFAC Symposium, 18-23 June, Ischia, Italy). Oxford, UK: Pergamon, pp. 202-5.
146. Thomson, W. (1988), Theory of Vibration with Applications. Englewood Cliffs, NJ: Prentice-Hall.
147. Unruh, J., Kana, F., Dodge, F., and Fey, T. (1986), "Digital Data Analysis Techniques for Extraction of Slosh Model Parameters," Journal of Spacecraft and Rockets 23(2): 171-7.
148. Weaver, W., Timoshenko, S., and Young, D. (1990), Vibration Problems in Engineering. New York: Wiley.
149. Williams, C. G. (1976), "Dynamics Modelling `and Formulation Techniques for Non-Rigid Spacecraft," Electronic and Space Systems, British Aircraft Corporation, Bristol, UK.
150. Williams, C., and Wood, T. (1989), "Dynamics and Formulation Techniques for Non-Rigid Spacecraft," ESTEC contract no. 8085/88/NL/MAC, TP9257, British Aircraft Corporation, Bristol, UK.
151. Dalquist, C. (1990), "Attitude Algebra Software: A Computer Tool for the Quaternion. Approach to Satellite Attitude Maneuvers," Paper no. 90-034, American Astro-nautical Society, San Diego, CA.
152. Goldstein, H. (1950), Classical Mechanics. Reading, MA: Addison-Wesley.
153. Hamilton, W. R. (1866), Elements of Quaternions. London: Longmans, Green.
154. Hildebrand, F. B. (1968), Methods of Applied Mathematics. New Delhi: Prentice-Hall.
155. Hughes, P. C. (1988), Spacecraft Attitude Dynamics. New York: Wiley.
156. Klumpp, A. R. (1976), "Singularity Free Extraction of a Quaternion from a Direction Cosine Matrix," Journal of Spacecraft and Rockets 13: 754-5.
157. Sabroff, A., Farrenkopf, R., Frew, A., and Gran, M. (1965), TRW Report AFFDL-TR-65-115, TRW, Redondo Beach, CA.
158. Wertz, J. (1978), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.
159. Bednarek, T. (1992), "Dual Cone Scanning Earth Sensor Processing Algorithms," Small Satellite Technologies and Applications II (SPIE vol. 1691). Bellingham, WA: International Society of Optical Engineering, pp. 181-91.
160. Desvignes, F., Doittau, F., Krebs, J., and Tissot, M. (1985), "Optical Sensors for Spacecraft Attitude Measurement with Respect to the Earth," Infrared Technology and Applications (SPIE vol. 590). Bellingham, WA: International Society of Optical Engineering, pp. 322-30.
161. Fallon, J., and Selby, V. (1990), "An Optical Locator for Horizon Sensing," Paper no. 90-32,13th Annual AAS Guidance and Control Conference (3-7 February, Keystone, CO).
162. Gates, F., and McAloon, K. (1976), "A Precision Star Tracker Utilizing Advanced Techniques," Paper no. 76-113, AIAA 14th Aerospace Sciences Meeting (January, Washington, DC).
163. Gontin, R. A., and Ward, K. A. (1987), "Horizon Sensor Accuracy Improvement Using. Earth Horizon Profile Phenomenology," Paper no. 87-2598, Navigation and Control Conference. Washington, DC: AIAA, pp. 1495-1502.
164. Hablani, H. (1993), "Modeling of Roll/Pitch Determination with Horizon Sensors: Oblate Earth," AIAA Guidance, Navigation and Control Conference (9-11 August, Monterey, CA). Washington, DC: AIAA, pp. 1133-47.
165. Hirshfeld, A., and Sinott, R. (1990), Sky Catalogue 2000.0. Belmont, MA: Sky Publishing.
166. Hoffleit, D. (1964), Catalog of Bright Stars. New Haven, CT: Yale University Observatory.
167. ITHACO, Inc. (1983), "Conical Earth Sensor (IPS-6) 12/83," ITHACO Space Products, Ithaca, NY.
168. Kosik, J. (1991), "Star Pattern Identification Aboard an Inertially Stabilized Spacecraft," Journal of Guidance, Control, and Dynamics 14(2): 230-5.
169. Lange, G., Mosbacher, B., and Purll, D. (1986), "The ROSAT Star Tracker," Instrumentation in Astronomy VI (SPIE vol. 627). Bellingham, WA: International Society of Optical Engineering, pp. 243-53.
170. Lyle, R., Leach, J., and Shubin, L. (1971), "Earth Albedo and Emitted Radiation," Document no. SP-8067, NASA, Washington, DC.
171. Matthews, A., Baker, R., and Doyle, C. (1992), "The Hemispherical Resonator Gyro: New Technology Gyro for Space," 12th FAC Symposium on Automatic Control in Aerospace: Aerospace Control 92 (7-11 September, Ottobrunn, Germany).
172. McCanless, F., Quasius, G., and Unruh, W. (1962), "Star Tracker Aerospace Reference Study-Stars," Report no. ASD-TDR-62-1056, Honeywell Military Products Group, St. Petersburg, FL.
173. Maute, P., Blancke, J., and Alby, F. (1989), "Autonomous Geostationary Station Keeping System Optimization and Validation," Acta Astronautica 20: 93-101.
174. McQuerry, J., Wagner, D., Sullivan, M., Deters, R., and Radovich, M. (1992), "A New Generation Stellar Attitude Sensor: The CT-601 Solid-State Star Tracker," 12th IFAC Symposium on Automatic Control in Aerospace: Aerospace Control 92 (7-11 September, Ottobrunn, Germany).
175. Muller, E., and Jappel, A. (1977), International Astronomical Union, Proceedings of the Sixteenth General Assembly (Grenoble 1976). Dordrecht: Reidel.
176. Pochard, M. (1992), "A Fifteen Years Lifetime Mechanism for an Infrared Earth Sensor" (ESA SP-334), Proceedings of the Fifth European Space Mechanisms and Tribol-ogy Symposium (28-30 October, ESTEC, Noordwijk, Netherlands). Paris: European Space Agency, pp. 353-8.
177. Sheela, B., Shekhar, C., Padmanabhan, P., and Chandrasekhar, M. (1991), "New Star Identification Technique for Attitude Control," Journal of Guidance, Control, and Dynamics 14(2): 477-80.
178. Sidi, M. (1980), "On Maximization of Gain-Bandwidth in Sampled Systems," International Journal of Control 32(6): 1099-1109.
179. Smithsonian Institute Staff (1971), Smithsonian Astrophysical Observatory Star Catalog, parts I-IV. Washington, DC.
180. SODERN (1977), "Static Infrared Horizon Sensor STA 03: Description, Operation, Functions and Characteristics," Document no. C.04.1163A, SODERN, Limeil-Brevannes, France.
181. SODERN (1991a), "Scanning Infrared Earth Sensor STD 15: Description, Operation, Functions and Characteristics," Document no. C.04.1346-05, SODERN, Limeil-Brevannes, France.
182. SODERN (1991b), "Infrared Horizon Scanning Sensor (500 to 1200 Km) STD 16: Description, Operation, Functions and Characteristics," Document no. C.04.1970-05, SODERN, Limeil-Brevannes, France.
183. Stanton, R., and Hill, R. (1980), "CCD Star Sensor for Fine Pointing Control of Space-borne Telescopes," Journal of Guidance and Control 3(2): 179-85.
184. Strikwerda, T., Fisher, H., Kilgus, C., and Frank, L. (1991), "Autonomous Star Identification and Spacecraft Attitude Determination with CCD Star Trackers," Spacecraft Guidance Navigation and Control Systems (proceedings of the first international conference organized by ESA at ESTEC, 4-7 June, Noordwijk, Netherlands). Paris: European Space Agency, pp. 195-200.
185. Swanson, C. (1982), "DRIRU 1/SKIRU-The Application of the DTG to Spacecraft Attitude Control," Paper no. 82-1624, AIAA Guidance and Control Conference (9-11 August, San Diego, CA).
186. Tai, F., and Barnes, R. (1989), "The Dual Cone Scanner: An Enhanced Performance, Low-Cost Earth Sensor," Paper no. 89-013,12th Annual AAS Guidance and Control Conference (4-8 February, Keystone, CO). San Diego, CA: American Astronautical Society, pp. 147-69.
187. Vedder, J. (1993), "Star Trackers, Star Catalogs, and Attitude Determination: Probabilistic Aspects of System Design," Journal of Guidance, Control, and Dynamics 16(3): 498-504.
188. Wertz, J. (1978), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.
189. Zwartbol, T., Van Den Dam, R., Terpstra, A., and Van Woerkom, P. (1985), "Attitude Estimation and Control of Maneuvering Spacecraft," Automatica 21(5): 513-26.
190. Agrawal, B. (1986), Design of Geosynchronous Spacecraft. Englewood Cliffs, NJ: Prentice-Hall.
191. Auer, W. (1992), "A Double Gimballed Momentum Wheel for Precision Three-Axis Attitude Control," IFAC Symposium on Automatic Control in Aerospace: Aerospace Control 92 (7-11 September, Ottobrunn, Germany). Oxford, UK: Perga-mon, pp. 581-6.
192. Azor, R. (1992), "Solar Attitude Control Including Active Nutation Damping in a Fixed-Momentum Wheel Satellite," Paper no. 92-4333, AIAA Guidance and Control Conference (10-12 August, Hilton Head Island, SC). Washington, DC: AIAA, pp. 226-35.
193. Berker, F. (1978), "MMS Propulsion Model Design," AIAA/SAE 14th Joint Propulsion Conference (25-27 July, Las Vegas, NV).
194. Bichler, U. (1991), "A Double Gimbaled Magnetic Bearing Momentum Wheel for High-Pointing Accuracy and Vibration Sensitive Space Applications," Spacecraft Guidance Navigation and Control Systems (proceedings of the first international conference organized by ESA at ESTEC, 4-7 June, Noordwijk, Netherlands). Paris: European Space Agency, pp. 393-8.
195. Bosgra, J., and Smilde, H. (1983), "Experimental and Systems Study of Reaction Wheels, Part I: Measurement and Statistical Analysis of Force and Torque Irregularities," NLF TR 82003 U, ESTEC, Noordwijk, Netherlands.
196. Duhamel, T., and Benoit, A. (1991), "New AOCS Concepts for ARTEMIS and DRS," Spacecraft Guidance Navigation and Control Systems (proceedings of the first international conference organized by ESA at ESTEC, 4-7 June, Noordwijk, Netherlands). Paris: European Space Agency, pp. 33-9.
197. Harris, C., and Kyrondis, G. (1990), "Effect of Thermal Radiation Torques on the TDRS," Paper no. 3492-CP, AIAA Guidance and Control Conference (20-22 August, Portland, OR). Washington, DC: AIAA, pp. 1602-14.
198. Lievre, J. (1985), "Solar Sailing Attitude Control of Large Geostationary Satellite," IFAC Automatic Control in Space. Oxford, UK: Pergamon.
199. Poeschel, R., and Hyman, J. (1984), "A Comparison of Electric Propulsion Technologies for Orbit Transfer," Hughes Research Laboratories, Malibu, CA.
200. Pritchard, W. L., and Sciulli, J. (1986), Satellite Communication Systems Engineering. Englewood Cliffs, NJ: Prentice-Hall.
201. Smith, P. (1988), "Design and Development of the UK-10 Ion Propulsion Subsystem," GDLR/AIAA/JSASS 20th International Electric Propulsion Conference (3-6 October, Garmisch-Partenkirchen, Germany).
202. Wertz, J. R. (1978), Spacecraft Attitude Determination and Control. Dordrecht: Reidel.
203. Wertz, J., and Larson, W. (1991), Space Analysis and Design. Dordrecht: Kluwer.