John E. Prussing
Professor Emeritus
of Aerospace Engineering
319a
Talbot Lab
(Directions to Talbot Lab)
(217) 333-8231
prussing@illinois.edu
http://prussing.ae.illinois.edu
330 Talbot Lab, MC-236
104 S. Wright St.
Urbana, IL 61801-2935
Department
of Aerospace
Engineering (AE)
Interesting
Links
Education
ScD, Instrumentation ,
Massachusetts
Institute of Technology (MIT),
1967
SM,
Aeronautics and Astronautics
(Honors Course ), MIT, 1963
SB, Aeronautics and Astronautics
(Honors Course), MIT, 1963
Experience
Professor Emeritus, Aerospace Engineering,
University of Illinois at Urbana-Champaign (UIUC),
2007–present
Professor, Aerospace Engineering,
University of Illinois at Urbana-Champaign (UIUC),
2003–2007
Professor, Aeronautical
& Astronautical
Engineering, University of Illinois at Urbana-Champaign (UIUC),
1981–2003.
Assistant Dean (half-time), College of Engineering, UIUC,
1976–77.
Associate Professor, Aeronautical & Astronautical Engineering,
UIUC, 1972–81.
Assistant Professor, Aeronautical & Astronautical Engineering,
UIUC, 1969–72.
Assistant Research Engineer and
Lecturer,
University
of California at San Diego,
1967–69.
Research
Interests
PRUSSING'S GOOGLE SCHOLAR CITATIONS
PRUSSING'S RESEARCH REFERENCED IN BOOKS & JOURNALS
Optimal spacecraft trajectories:
The study of optimal
(minimum-propellant) spacecraft trajectories
is an important
research area in the general field of
astrodynamics.
Each kilogram of propellant saved by optimizing the trajectory results
in
an additional kilogram (or more)
of payload delivered to the final destination. The
trajectory being optimized may represent an orbital rendezvous or
interception,
or an orbit transfer.
There are two basic types of
spacecraft propulsion systems: high thrust
and low thrust. In high-thrust
systems the engine operates only during
very brief time intervals. In this case the thrusts can be approximated
by impulses. The times and directions of these thrust impulses can be
determined
so that propellant consumption is minimized and the desired final orbit
conditions are satisfied.
In low-thrust systems the engine is either on continuously or switches
on
and off for long time intervals, depending on whether the propulsion
system
is constant specific impulse (CSI) or variable specific impulse (VSI),
sometimes called power limited (PL).
In the CSI case the continuously-varying thrust direction
and
the on-off switching times can be determined.
In the VSI
case
the continuously-varying thrust direction and magnitude can be
determined
to minimize the propellant consumption and satisfy the desired final
orbit
conditions.
Research interests include:
Earth escape using a solar sail (funded by
NASA
Jet Propulsion Laboratory )
Applications
of second-order necessary conditions and sufficient conditions in optimal control
problems
Investigation of a closed-form optimal VSI
thrust program for a spacecraft trajectory in an arbitrary gravitational
field
Optimal cooperative rendezvous
Geocentric and heliocentric applications of solar sails
At
a Glance
Professor Prussing
taught the following UIUC courses:
Undergraduate:
AE
100 Intro
Aerospace Engineering(formerly AE 199) Course Web Page
AE
201 Aerospace
Systems Principles Web Page for Spaceflight
Segment
AE
302 Aerospace
Flight Mechanics Web Page
Undergraduate/Graduate:
AE
402 Orbital
Mechanics Course Web Page
AE
403
Spacecraft Attitude Control
Course
Web Page
Graduate:
AE
504 Optimal
Aerospace Systems Course Web Page
AE
508 Optimal
Space Trajectories Course Web Page
Prof. Prussing and Prof.
B.
A. Conway,
of the AE Department are co-authors of the
textbook for AE 402,
Orbital Mechanics
published
by Oxford University Press. The First Edition is owned by 293
public and university
libraries
worldwide in 44 states of the U.S., 9 provinces of Canada, and in
Australia (9), China, France, Germany (8), Greece, Hong Kong,
Ireland, Israel,
New Zealand, Singapore, South Africa, Spain and the United Kingdom (14).
A Second and expanded edition was published in 2013.
It is owned by public and university libraries in the
U.S. and Canada, and in New Zealand, Taiwan, Turkey, and the U.K.
Books that cite Prussing & Conway
Orbital Mechanics, First Edition
The most recent Errata
for the First Edition
exists as a
PDF file
Errata.1ed.pdf
.
The most recent Errata for the Second
Edition is at
Errata.2ed.pdf
.
For more information on the First Edition
see the detailed
Table of Contents and the Preface.
Also
amazon.com shows selected
pages and reviews.
For more information on the Second Edition
see the detailed
Table of Contents and the Preface.
Also
amazon.com shows selected
pages and reviews.
Professor Prussing has published over 50
archival
research articles in 13
different
technical
journals These articles are referenced in
62 different journals in English and also in
journals in Russian, Chinese, French, and Portuguese.
He has presented a
two-day short course
"Optimal
Orbital Maneuvers" three times:
AAS/AIAA Astrodynamics Conference in Stowe,Vermont, 1989
NASA Lewis (now Glenn) Research Center/Analex Corp. in Cleveland, Ohio
, 1989
NASA Goddard Space Flight Center, 2002
Here is an
administrative biosketch for the American Association
of University Professors (AAUP)
Honors and Awards:
Elected
Fellow
of the American Institute of
Aeronautics and Astronautics (AIAA)
"for outstanding contributions to astrodynamics research and education,
and for service to the aerospace community."
(1994)
Elected
Fellow
of the American Astronautical
Society
(AAS)
"for contributions that have made a significant impact on the fields
of space flight mechanics and astronautics."
(1997)
Received the
Mechanics and Control Award
of the AIAA
"For an outstanding contribution to the theory and computation
of optimal spacecraft trajectories by developing a practical,
necessary and sufficient condition test for optimality."
(2002)
Received the
Dirk Brouwer Award of the AAS
"For exceptionally significant contributions
to the literature of orbital mechanics, particularly in research in
optimal
spacecraft trajectories." (1994)
Best Paper Award
of the
AAS/AIAA Space Flight Mechanics
Meeting, Feb. 1998, Monterey,
California
Associate
Editor of the AIAA
Journal
of Guidance, Control, and Dynamics
1989–92
Chair
of the
AIAA
Astrodynamics Technical Committee
1982–84; Member 77–80, 81–84,
87–90
Member of the AAS
Space Flight Mechanics Committee
1980–96
Member of Sigma Xi, Scientific Research Honorary Society
Member of Sigma Gamma Tau, Aerospace Engineering Honorary Society
Member of The Order of the Engineer
Finalist 2 times for the UIUC
Campus Award
for Excellence in Undergraduate Teaching
Named 23 semesters on
A
List of Teachers Ranked as Excellent by Their Students,
most recently for
Spring 2010 (AE 508),
Spring 2009 (AE 403), Spring 2008 (AE 508), and
Fall 2007 (AE 402).
Voted AE Department Teacher of
the Year 5 times by the students
Received
Engineering Council (Accenture) Award for Excellence in
Advising 15 times 1989–2008, as voted by
the students.
Books,
Chapters in Books, Monographs, Book Reviews
Optimal Spacecraft Trajectories by John E. Prussing, Oxford University
Press, 2018.
An Errata file is at Errata.OST.pdf
Optimal Control with Aerospace Applications
by
James M. Longuski, Jose' J. Guzman, and John E. Prussing, Springer USA and
Microcosm Press, 2013. It is owned by 211 university and public libraries
worldwide,
including Australia, Belgium, Canada (8 provinces),
Denmark, Germany, Hong Kong, Italy, Japan, Korea, Luxembourg, Malaysia,
Netherlands, New Zealand, Norway, Peru, Qatar, Singapore, Spain,
Sweden, United Arab Emirates, and the U.K.
"Primer Vector Theory and Applications", Chapter 2 in
Spacecraft Trajectory Optimization (B.A. Conway, editor) Cambridge
University Press, 2010. It is owned by 347 university and public libraries
wordwide, including Canada, Germany, Hong Kong, Japan, Namibia, South Africa,
Taiwan, Turkey, United Arab Emirates, and the U.K.
Orbital
Mechanics
by John E. Prussing and
Bruce
A. Conway,
Oxford University Press, 1993, Second Edition 2012 (See above for details and errata.)
Optimal Orbital Maneuvers, AIAA
Professional Study Series, 1989.
"Kepler's
Laws of Planetary Motion ",
Encyclopedia
of Physics, 3rd
Edition, Van Nostrand Reinhold Co., 1990.
Prussing's doctoral thesis
Optimal Multiple-Impulse Orbital Rendezvous.
Published
Book Reviews
Technical
Reviews
Selected
Journal Articles
Prussing, J.E.,
"Simplified Conjugate Point Procedure",
Journal of Guidance, Control, and Dynamics,,
Vol. 40, No. 5, May 2017, pp. 1255–1257.
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.
[Also Presented as
Paper
AIAA 2002-4726, AIAA/AAS
Astrodynamics Specialists Conference, Monterey, CA, August 2002.]
"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.]
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, pp. 628–634, Jul–Aug 2003.
See related
UIUC News Bureau news article
and
Science
Daily news article
[Presented at the AAS/AIAA Astrodynamics Specialist Conference,
Girdwood, AK, August 1999, Paper No. AAS 99–333. 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].
"
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.]
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, pp. 241–250.
[This journal article is a condensed version of two conference
papers
presented at the 8th
AAS/AIAA Space Flight Mechanics Meeting,
Monterey, CA, Feb. 1998, Paper
Nos. AAS 98–163 and 98–164.
Paper No. 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, Eds. J. W. Middour
et al, Univelt Inc., San Diego, CA]
Prussing, J. E., and
Coverstone-Carroll,
V., "
Constant Radial Thrust Acceleration Redux,"
Journal
of Guidance, Control, and Dynamics,
Vol. 21, No. 3,
May–Jun 1998, pp. 516–518.
[Presented at the AIAA/AAS
Astrodynamics Specialists Conference,
Boston, MA, Aug. 1998,
Paper No. AIAA 98–4545.]
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.]
"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.]
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.]
All
Journal Articles
UIUC Engineering Hall
Graduate
Students
Professor
Prussing has been thesis
advisor for 33 M.S. students and 9 Ph.D.
students.
Ph.D. Degrees, Thesis Title, and
Student Placement, Current Position
9. Suzannah L. Sandrik,
"Primer-Optimized Results and Trends for
Circular Phasing and Other Circle-To-Circle Impulsive Coplanar
Rendezvous " (2006), Associate Faculty Associate in Engineering
Physics, University of
Wisconsin at Madison.
8. Jang-Won Jo,
" Applications
of Second-Order
Necessary and Sufficient Conditions to Optimal Trajectories "
(1997), Postdoctoral Research Associate, University of Illinois at
Urbana-Champaign. Currently, Republic of Korea Ministry of National
Defense.
7.
Victoria
Coverstone-Carroll ,
" Optimal
Cooperative Power-Limited Rendezvous
" (1992), Engineering
Faculty, University of Illinois at Urbana-Champaign. Currently,
Professor of Aerospace
Engineering & Associate Dean of Engineering,
University of Illinois at Urbana-Champaign.
6. Der-Ren Taur,
" Optimal
Multiple-Impulse
Rendezvous and Interception with Path Constraints "
(1989),
Chung Shan Institute of Science and Technology (CSIST),Taiwan, R.O.C.
5. William G. Heckathorn.
"
Optimal Multiple-Impulse
Direct-Ascent Time-Fixed Interception "
(1985), U.S. Air Force,
Wright-Patterson AFB. Currently, Colonel U.S. Air Force (Ret)
4. Jeng-Hua Chiu.
" Optimal
Multiple-Impulse
Nonlinear Orbital Rendezvous "
(1984), Colonel R.O.C. Air Force,
Chung Shan Institute
of Science and Technology (CSIST), Taiwan, R.O.C.
3. Steven J. Hoffman,
" An
Optimization Method
for the Preliminary Design of Interplanetary Aerobraking Missions "
(1984), Science Applications International Corp. (SAIC), Schaumburg,IL.
Currently, SAIC, Houston,TX.
2. Ting-Nung Shiau,
" Rotor
Blade Flap-Lag
Stability and Response in Forward Flight in Turbulent Flows "
(1984), Faculty, Institute of Aeronautics and Astronautics, National
Cheng
Kung University, Taiwan, R.O.C.
Currently, Professor Emeritus of Mechanical Engineering, National Chung Cheng University,
Taiwan, R.O.C.
1. Larry R. Gross,
" Optimal
Multiple-Impulse
Direct-Ascent Rendezvous "
(1972), U.S. Air Force, Wright-Patterson
AFB.
M.S. Degrees, Thesis Title, and
Student Placement (1993–Present)
34. Kaushik Ponnapalli
"
Optimal Variable-Specific-Impulse
Trajectories in Simple Gravitational Fields
" (2019), Vantage Partners LLC,
Cleveland, OH.
33. Eamon E. McCleery,
"
Optimal
Impulsive Transfers between Non-Coplanar
Circular Orbits Using the Primer Vector
" (2004), Northrup Grumman
Corporation, Los Angeles, CA.
32. Suzannah L. Sandrik,
"
Analysis
of Kechichian's Optimal Control Solution to
a Low-Thrust Orbit Transfer Problem"
(2002), Ph.D. Program,
UIUC AAE.
31. Michael C. Tanzillo,
"
Optimal
Escape Using Low Thrust Trajectories
" (2000), The Aerospace
Corporation, El Segundo, CA.
30. Chad M. Sund,
" Velocity
Feedback Control
for Optimal Power-Limited Trajectories "
(1996), U. S. Marine
Corps Flight School, Pensacola, FL.
29. Jeffrey P. Elbel,
" Multiple
Revolution
Solutions to Lambert's Problem using Laguerre's Algorithm "
(1993), Hughes Aerospace Corporation, Los Angeles, CA. Currently,
Editor, Space Times Magazine, American Astronautical Society
28. Timothy J. Urban,
" Optimal
Thrust-Limited
Path-Constrained Rendezvous in a Linearized Gravitational Field "
(1993), Ph.D. Program, University of Texas at Austin.
Earlier
(pre-1993) M.S. Thesis Students
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Last update 12 dec 2019