54. Prussing, J.E., "Simplified Conjugate Point Procedure, "Journal of Guidance, Control, and Dynamics, Vol. 40, No. 5, May 2017, pp. 1255–1257.
53. Prussing, J.E., and Sandrik, S.L., " Second-Order Necessary Conditions and Sufficient Conditions Applied to Continuous-Thrust Trajectories,"Journal of Guidance, Control, and Dynamics, Vol. 28, No. 4, Jul–Aug 2005, pp. 812–816
[Presented as Paper No. AIAA 2002-4726, AIAA/AAS Astrodynamics Specialist Conference, Monterey, CA, August 2002.]
52. "Optimal Two- and Three-Impulse Fixed-Time Rendezvous in the Vicinity of a Circular Orbit", Journal of Spacecraft and Rockets, Vol. 40, No. 6, Nov–Dec 2003, pp. 952–959 [ Reprinted from AIAA Journal, Vol. 8, No. 7, 1970 as part of an Historical Celebration.]
51. Coverstone, V. L. , and Prussing, J. E., Technique for Earth Escape from Geosynchronous Transfer Orbit Using a Solar Sail Journal of Guidance, Control, and Dynamics, Vol. 26, No. 4, Jul–Aug 2003, pp. 628–634
[Presented at the AAS/AIAA Astrodynamics Conference, Girdwood, Alaska, Aug 1999, Paper No. 99-333.]
50. " A Class of Optimal Two-Impulse Rendezvous Using Multiple-Revolution Lambert Solutions, " The Journal of the Astronautical Sciences , Vol. 48, Nos. 2 and 3, Apr-Sep 2000, pp. 131–148. Also appears in Advances in the Astronautical Sciences, Vol. 106, pp. 17–39, Eds. J.L. Junkins et al, Univelt Inc., San Diego, CA.
[Presented at The Richard H. Battin Astrodynamics Symposium, College Station, TX, March 2000, Paper No. AAS 00-250.]
49. Jo, J-W., and Prussing, J. E., " Procedure for Applying Second-Order Conditions in Optimal Control Problems, " Journal of Guidance, Control, and Dynamics , Vol. 23, No. 2, Mar–Apr 2000.
[This journal article is a condensed version of two papers presented at the 8th AAS/AIAA Space Flight Mechanics Meeting, Monterey, CA, Feb. 1998, Paper Nos. AAS 98-163 and AAS 98-164.]
[Paper AAS 98-163 received the Best Paper Award for the conference.]
[The conference papers appear in Advances in the Astronautical Sciences Vol. 99, Part II, pp. 865–881 and 883–905, Ed. J. W. Middour et al, Univelt Inc., San Diego CA.]
48. Powers, R. B., Coverstone-Carroll, V. , and Prussing, J. E., "Solar Sail Optimal Transfers to Synchronous Orbits"".
[Presented at the AAS/AIAA Astrodynamics Conference, Girdwood, Alaska, Aug 1999, Paper No. 99-334.]
Also appears in Advances in the Astronautical Sciences Vol. 103, Part I, pp. 523–537, Eds. K. C. Howell et al., Univelt Inc., San Diego, CA.
47. Prussing, J. E., and Coverstone-Carroll, V., "Constant Radial Thrust Acceleration Redux," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 4, Jul-Aug, 1998, pp. 516-518.
[A slightly expanded version was later presented at the AIAA/AAS Astrodynamics Specialists Conference, Boston, MA, Aug. 1998, Paper No. AIAA 98-4545.]
46. "Terminal Maneuver for an Optimal Cooperative Impulsive Rendezvous", Advances in the Astronautical Sciences, Vol. 97, Part I, pp. 759-772, Eds. Felix Hoots et al., Univelt Inc., San Diego, CA.
[Presented as Paper No. AAS 97-649, AAS/AIAA Astrodynamics Conference, Sun Valley, ID, August 1997.]
45. Wenzel, R. S., and Prussing, J. E., "A Preliminary Study of Optimal Thrust-Limited Path-Constrained Maneuvers", Journal of Guidance, Control, and Dynamics, Vol. 19, No. 6, Nov-Dec 1996, pp. 1303-1309.
[Presented as Paper No. AAS 91-133, AAS/AIAA Spaceflight Mechanics Meeting, Houston, TX, February 1991.]
44. "Closed-Form Thrust Acceleration for Optimal Power-Limited Trajectories", Advances in the Astronautical Sciences, Vol. 93, Part II, pp. 1517-1528, Eds. R.H. Bishop et al., Univelt Inc., San Diego, CA.
[Presented as Paper No. AAS 96-198, AAS/AIAA Space Flight Mechanics Conference, Austin, TX, February 1996]
43. Coverstone-Carroll, V., and Prussing, J. E.,"Optimal Cooperative Power-Limited Rendezvous with Propellant Constraints", The Journal of the Astronautical Sciences, Vol. 43, No. 3, Jul-Sep 1995, pp. 289-305.
[Presented as Paper No. AIAA 92-4508, AIAA/AAS Astrodynamics Conference, Hilton Head, SC, August 1992.]
42. "Optimal Impulsive Linear Systems: Sufficient Conditions and Maximum Number of Impulses", The Journal of the Astronautical Sciences, Vol. 43, No. 2, Apr-Jun 1995, pp. 195-206.
[Presented as Paper No. 94-174, AIAA/AAS Spaceflight Mechanics Meeting, Cocoa Beach, FL, February 1994.]
41. "Optimal Power-Limited Trajectories in an Arbitrary Gravitational Field", Advances in the Astronautical Sciences, Vol. 89, Part II, pp. 1045-1060, Eds. R. J. Proulx et al., Univelt Inc., San Diego, CA.
[Presented as Paper No. AAS 95-216, AAS/AIAA Space Flight Mechanics Conference, Albuquerque, NM, February 1995]
40. Taur, D.-R. Coverstone-Carroll, V. and Prussing, J. E., "Optimal Impulsive Time-Fixed Orbital Rendezvous and Interception with Path Constraints", Journal of Guidance, Control, and Dynamics, Vol. 18, No. 1, Jan-Feb 1995, pp. 54-60.
[Presented as Paper No. AAS 90-2971, AIAA/AAS Astrodynamics Conference, Portland, OR, August 1990.]
39. Coverstone-Carroll, V., and Prussing, J. E., "Optimal Cooperative Power-Limited Rendezvous Between Coplanar Circular Orbits", Journal of Guidance, Control, and Dynamics,Vol. 17, No. 5, Sep-Oct 1994, pp. 1096-1102.
[Presented as Paper No. AAS 91-444, AAS/AIAA Astrodynamics Specialist Conference, Durango, CO, August 1991.]
38. Prussing, J. E. and Clifton, R. S., "Optimal Multiple-Impulse Satellite Evasive Maneuvers," Journal of Guidance, Control, and Dynamics, Vol. 17, No. 3, May-Jun 1994, pp 599-606.
[Presented as Paper No. 87-543, AAS/AIAA Astrodynamics Conference, Kalispell, MT, August 1987.]
37. Coverstone-Carroll, V. and Prussing, J. E., " Optimal Cooperative Power-Limited Rendezvous Between Neighboring Circular Orbits", Journal of Guidance, Control, and Dynamics, Vol. 16, No. 6, Nov-Dec 1993, pp. 1045-1054.
[Presented as Paper No. AAS 91-444, AAS/AIAA Astrodynamics Specialist Conference, Durango, CO, August 1991.]
36. Lembeck, C. A.and Prussing, J. E., "Optimal Impulsive Interception with Low-Thrust Rendezvous Return," Journal of Guidance, Control, and Dynamics, Vol. 16, No. 3, May-Jun 1993.
[Presented as Paper No. AAS 89-354, AAS/AIAAA Astrodynamics Specialist Conference, Stowe, VT, August 1989.]
35. "Equation for Optimal Power-Limited Spacecraft Trajectories", Journal of Guidance, Control, and Dynamics, Vol. 16, No. 2, Mar-Apr 1993, pp. 391-393.
[Presented as Paper No. AAS 93-147, AAS/AIAA Spaceflight Mechanics Meeting, Pasadena, CA, February 1993.]
34. " Simple Proof of the Global Optimality of the Hohmann Transfer ", Journal of Guidance, Control, and Dynamics, Vol. 15, No. 4, July-August, 1992, pp. 1037-38
33. Ochoa, S. I., and Prussing, J. E., " Multiple Revolution Solutions to Lambert's Problem ", Advances in the Astronautical Sciences, Vol. 79, Part II, pp. 1989-2008, Eds. B. Kaufman et al., Univelt Inc., San Diego, CA.
[ Presented as Paper No. 92-194, AAS/AIAA Spaceflight Mechanics Meeting, Colorado Springs CO, February 1992.]
32. Sri Namachchivaya, N. and Prussing, J. E., " Almost-Sure Asymptotic Stability of Rotor Blade Flapping Motion in Forward Flight in Turbulent Flows, "Probabilistic Engineering Mechanics, Vol. 6, No. 1, pp. 2-9, March 1991.
31. Prussing, J. E. and Conway. B. A., " The Optimal Terminal Maneuver for a Cooperative Impulsive Rendezvous, " Journal of Guidance, Control and Dynamics, Vol. 12, No. 3, May-Jun 1989, pp. 433-435, (also Errata Vol. 12, No. 4, p. 608).
30. Prussing, J. E., Wellnitz, L. J, and Heckathorn, W. G., "Optimal Impulsive Time-Fixed, Direct-Ascent Interception, " Journal of Guidance, Control and Dynamics, Vol. 12, No. 4, Jul-Aug 1989, pp. 487-494.
[Presented as Paper No. 87-539, AAS/AIAA Astrodynamics Conference, Kalispell, MT, August 1987.]
29. Shiau, T. N., Prussing, J. E., and Lin, Y. K., " Fourier Matrix Product with Application to the Rotor Blade Random Vibration, " Journal of the Chinese Society of Mechanical Engineers, Vol. 7, No. 4, 1986, pp. 217-225.
28. " The Principal Minor Test for Semidefinite Matrices ", Journal of Guidance, Control and Dynamics, Vol. 9, No. 1, Jan-Feb 1986, pp. 121-122.
27. Prussing, J. E., and Chiu, J-H., " Optimal Multiple Impulse Time-Fixed Rendezvous Between Circular Orbits ", Journal of Guidance, Control and Dynamics, Vol. 9, No. 1, Jan-Feb 1986, pp. 17-22, (also Errata, Vol. 9, No. 2, p. 255). [also appears in Russian translation in Aerokosmichekaya Techanika , No. 8, 1986, pp. 135-142 (U.S.S.R).]
[Presented as Paper No. 84-2036, AIAA/AAS Astrodynamics Conference, Seattle, WA, August 1984.]
26. Prussing, J. E., Lin, Y. K., and Shiau, T. N., " Rotor Blade Flap-Lag Stability and Response in Forward Flight in Turbulent Flow, " Journal of the American Helicopter Society, Vol. 29, No. 4, Oct. 1984, pp. 81-87.
25. Prussing, J. E., and Lin, Y. K., " A Closed-Form Analysis of Rotor Blade Flap-Lag Stability in Hover and Low Speed Forward Flight in Turbulent Flow, " Journal of the American Helicopter Society, Vol. 28, No. 3, July 1983, pp. 42-46.
[Presented at the AIAA/ASME/ASCE/AHS 24th Structures, Structural Dynamics and Materials Conference, Lake Tahoe, NV, May 1983.]
24. Fuh, J.S., Hong, C. Y. R., Lin, Y. K., and Prussing, J. E.," Coupled Flap Torsional Response of a Rotor Blade in Forward Flight due to Atmospheric Turbulence Excitations ", Journal of the American Helicopter Society, Vol. 28, No. 3, July 1983, pp. 3-12.
23. Bergam, M. J., and Prussing, J. E., " Comparison of Starting Values for Iterative Solutions to a Universal Kepler's Equation, " Journal of the Astronautical Sciences, Vol. 30, No. 1, pp. 75-84, Jan.-Mar. 1982.
22. Lin, Y. K., and Prussing, J. E., " Concepts of Stochastic Stability in Rotor Dynamics, " Journal of the American Helicopter Society, Vol. 27, No. 2, pp. 73-74, April 1982.
21. Prussing, J. E., and Lin, Y. K., " Rotor Blade Flap-Lag Stability in Turbulent Flows, " Journal of the American Helicopter Society, Vol. 27, No. 2, pp. 51-57, April 1982.
20. " Orthogonal Multiblade Coordinates, " Journal of Aircraft, Vol. 18, No. 6, pp. 504-506, June 1981.
19. " Stabilization of an Unstable Linear System by Parametric White Noise ", Journal of Applied Mechanics, Vol. 48, No. 1, pp. 198-199, March 1981.
18. " Bounds on the Solution to a Universal Kepler's Equation, " Journal of Guidance and Control, Vol. 2, No. 5, pp. 440-442, Sept.-Oct. 1979.
17. " A Geometric Interpretation of the Angles Alpha and Beta in Lambert's Problem, " Journal of Guidance and Control, Vol. 2, No. 5, pp. 442-443, Sept.-Oct. 1979.
16. " A Class of Nonlinear Systems Having Constant Optimal Control ", International Journal of Control, Vol. 28, No. 3, September 1978, pp. 329-331.
15. Prussing, J. E., and Krier, H., " Transient Temperature Response of Charring Composite Slabs ", International Journal of Heat and Mass Transfer, Vol. 21, No. 4, April 1978, pp. 519-22.
14. " The Mean Radius in Kepler's Third Law, " American Journal of Physics, Vol. 45, No. 12, December 1977, pp. 1216-1217.
13. " How to Serve in Tennis, " The Mathematical Gazette, Vol. 61, No. 418, December 1977, pp. 294-96.
12. " Bounds on the Solution to Kepler's Problem, " Journal of the Astronautical Sciences, Vol. 25, No. 2, Apr-Jun 1977, pp. 123-128.
[Presented at the AIAA/AAS Atrodynamics Conference, Palo Alto CA, August 1978.]
11. Prussing, J. E., and Wiley, J. C., " An Iterative Procedure for Determining Limit Cycles Using Lagrangian Mechanics, " AIAA Journal, Vol. 14, No. 3, March 1976, pp. 320-326.
10. " The Brachistochrone-Tautochrone Problem in a Homogeneous Sphere, " American Journal of Physics, Vol. 44, No. 3, 1976, pp. 304-305.
9. Gross, L. R., and Prussing, J. E., "Optimal Multiple-Impulse Direct Ascent Fixed-Time Rendezvous, " AIAA Journal,Vol. 12, No. 7, July 1974, pp. 885-889.
[Presented at the AAS/AIAA Astrodynamics Conference, Vail CO, July 1973.]
8. " A Nonrelativistic Analogy to Relativistic Time Dilatation, " The Mathematical Gazette, Vol. LVI, No. 397, October 1972, pp. 197-199.
7. " A Simplified Method for Solving the Matrix Riccati Equation, " International Journal of Control, Vol. 15, No. 5, May 1972, pp. 995-1000.
6. " Optimal Two- and Three-Impulse Fixed-Time Rendezvous in the Vicinity of a Circular Orbit", AIAA Journal, Vol. 8, No. 7, July 1970, pp. 1221-1228. [also appears in Russian in Raketnaya Techanika i Kosmonavtika, Vol. 7, 1970, pp. 46-56 (U.S.S.R.)]
5. Schneider, A. M., Prussing, J. E., and Timin, M., " A Manual Method for Space Rendezvous Navigation and Guidance, "Journal of Spacecraft and Rockets, Vol. 6, No. 9, September 1969, pp. 998-1106.
[Presented as Paper No. 68-859, AIAA Guidance, Control, and Flight Dynamics Conference, Pasadena CA, August 1968.]
4. " An Illustration of the Primer Vector in Optimal Time-Fixed Impulsive Transfer. " AIAA Journal , Vol. 7, No. 6, June 1969, pp. 1167-1168.
3. " Optimal Four-Impulse Fixed-Time Rendezvous in the Vicinity of a Circular Orbit ", AIAA Journal, Vol. 7, No. 5. May 1969, pp. 928-935. [also appears in Russian in Raketnaya Techanika i Kosmoavtika, No. 5, 1969, pp. 163-172 (U.S.S.R)]
2. " Obtaining Real Solutions for Nonlinear Systems Using Certain Transformation Techniques ", International Journal of Control, Vol. 9, No. 3, March 1969, pp. 359-362.
1. Hollister, W. M., and Prussing, J. E., " Optimum Transfer to Mars via Venus" " Astronautica Acta, Vol. 12, No. 2, Mar-Apr 1966, pp. 169-179.
[Presented at the AIAA/ION Astrodynamics Specialist Conference, Monterey CA, September 1965.]