E. Bruce Jackson

Note: links to papers served by the NASA Technical Report server (with handle.net URLs) often break, as this method of naming seems a bit volatile and is beyond my control; I'll attempt to fix them as I find them to be changed.

Bibliography (in reverse chronological order)

  1. Bailey, Randall E.; Jackson, E. Bruce; Goodrich, Kenneth H.; Ragsdale, W. Al; Neuhaus, Jason; and Barnes, Jim: Initial Investigation of Reaction Control System Design on Spacecraft Handling Qualities for Earth Orbit Docking. J. Guidance, Control and Dynamics, vol. 32, no. 6, November-December 2009.
  2. Hildreth, Bruce; and Jackson, E. Bruce: Benefits to the Simulation Training Community of a New ANSI Standard for the Exchange of Aero Simulation Models. To be presented at the 2009 Interservice/Industry Training Systems Conference, Orlando, FL, December 2009.
  3. Bailey, Randall E.; Jackson, E. Bruce; Bilimoria, Karl D.; Mueller, Eric R.; Frost, Chad R.; and Aldrete, Thomas S.: Cooper-Harper Experience Report for Spacecraft Handling Qualities Applications. NASA/TM-2009-215767, 2009
  4. Bailey, Randall E.; Jackson, E. Bruce; Goodrich, Kenneth H.; Ragsdale, W. Al; Neuhaus, Jason; and Barnes, Jim: Initial Investigation of Reaction Control System Design on Spacecraft Handling Qualities for Earth Orbit Docking. AIAA Paper 2008-6553. Presented at the AIAA Atmospheric Flight Mechanics Conference, 19 August 2008, Honolulu, Hawaii. Presentation slides are available here. [Paper also available here]
  5. Schutte, Paul C.; Goodrich, Kenneth H.; Cox, David E.; Jackson, E. Bruce; Palmer, Michael T.; Pope, Alan T.; Schlecht, Robin W.; Tedjojuwono, Ken K.; Trujillo, Anna C.; Williams, Ralph, A.; Kinney, J. Bryan; and Barry, John S., Jr.: The Naturalistic Flight Deck System: An Integrated System Concept for Improved Single-Pilot Operations. NASA TM-2007-215090 . [Paper available here]
  6. McMinn, J. D.; Jackson, E. Bruce; and Christhilf, David M.: Simulation Environment for Orion CEV Launch Abort Control Design Studies. AIAA Paper 2007-6881. Presented at the AIAA Modeling and Simulation Technologies Conference, 23 August 2007, Hilton Head, South Carolina. Presentation slides are available here. [Paper also available here]
  7. Hill, Melissa A.; and Jackson, E. Bruce: The DaveMLTranslator: An Interface for DAVE-ML Aerodynamic Models. AIAA Paper 2007-6890. Presented at the AIAA Modeling and Simulation Technologies Conference, 23 August 2007, Hilton Head, South Carolina. Presentation slides are available here. [Paper also available here]
  8. Jackson, E. Bruce; and Buttrill, C. W.: Control Laws for a Wind Tunnel Free-Flight Study of a Blended-Wing-Body Aircraft. NASA/TM-2006-214501, August 2006.
    [Also available here]
  9. Jackson, E. Bruce; and Hildreth, Bruce L.: Progress Toward a Format Standard for Flight Dynamic Models. Paper for and presentation to the Fall 2006 Simulation Interoperability Workshop, September 2006, Orlando, Florida.
  10. Jackson, E. Bruce: Using the Proposed AIAA Aerodynamic Modeling Standard (AeroML) or How to build a portable sim. Presentation to a special workshop at the AIAA Modeling and Simulation Technology Conference, 21 August 2006, Keystone, Colorado.
  11. Jackson, E. Bruce: DAVE-ML: The Proposed Implementation of the Simulation Standard for Model Exchange Presentation to a special workshop at the AIAA Modeling and Simulation Technology Conference, August 2005, San Francisco, California.
  12. Jackson, E. Bruce; Hildreth, Bruce L.; York, Brent W.; and Cleveland, William: Evaluation of a Candidate Flight Dynamics Model Simulation Standard Exchange Format. AIAA Paper 2004-5038. presented at the AIAA Modeling and Simulation Technologies Conference and Exhibit, 17 August 2004, Providence, Rhode Island.
  13. Raney, David L.; Jackson, E. Bruce; and Buttrill, Carey S.: Simulation Study of Impact of Aeroservoelastic Characteristics on Flying Qualities of a High Speed Civil Transport. NASA/TP-2002-211943, October 2002. [Also available here.]
  14. McMinn, J. D. and Jackson, E. Bruce: Autoreturn Function for a Remotely Piloted Vehicle. AIAA Paper 2002-4673. Presented at the AIAA Guidance, Navigation and Control Conference, 6 August 2002, Monterey, California.
    [Also available here]
  15. Jackson, E. Bruce and Hildreth, Bruce L.: Flight Dynamic Model Exchange using XML. AIAA Paper 2002-4482. Presented at the AIAA Modeling and Simulation Technology Conference, 5 August 2002, Monterey, California.
    [Also available here.]
    [Note: this project has garnered additional interest; see the DAVE-ML web site for more information.]
  16. Jackson, E. Bruce; Raney, David L.; Glaab, Louis J.; and Derry, Stephen D.: Piloted Simulation Assessment of a High-Speed Civil Transport Configuration. NASA/TP-2002-211441, March 2002.
  17. Raney, David L.; Jackson, E. Bruce; Buttrill, Carey S.; and Adams, William M.: The Impact of Structural Vibration on Flying Qualities of a Supersonic Transport. AIAA Paper 2001-4006. Presented at the AIAA Atmospheric Flight Mechanics Conference, 6 August 2001, Montreal, Canada.
  18. Rivers, Robert A.; Jackson, E. Bruce; Fullerton, C. Gordon; Cox, Timothy H.; and Princen, Norman H.: A Qualitative Piloted Evaluation of the Tupolev Tu-144 Supersonic Transport. NASA/TM-2000-209850, February 2000.
    [Paper also available here.]
  19. Jackson, E. Bruce; Raney, David L.; Hahne, David E.; Derry, Stephen D.; and Glaab, Louis J.: Reference H Piloted Assessment (LaRC.1) Pilot Briefing Guide. NASA/TM-1999-209533, December 1999.
    [Also available here.]
  20. Jackson, E. Bruce; Martínez, Debbie; and Derry, Stephen D.: Piloted Simulation Investigation of a Supersonic Transport Configuration (LaRC.4). NASA/TM-1999-209557, September 1999.
    [Paper also available here.]
  21. Rivers, Robert A., and Jackson, E. Bruce: Russian Tu-144 Supersonic Transport Flight Test. Presented to the 15th Annual East Coast Symposium of the Society of Experimental Test Pilots, Solomons, MD, April 15, 1999.
  22. Jackson, E. Bruce; and Rivers, Robert A.: Flight-Simulated Launch-Pad-to-Landing Abort Maneuvers for a Lifting Body. AIAA Paper 98-4254. Presented at AIAA Atmospheric Flight Mechanics Conference, Boston, MA, August 10-12, 1998.
    [Also available here.]
  23. Raney, David L. and Jackson, E. Bruce: Effect of Engine Response Time and Other Factors on Landing of a Supersonic Transport in the Backside Flight Regime. NASA TP-3632, April 1997.
  24. Jackson, E. Bruce: Results of a Flight Simulation Software Methods Survey. AIAA Paper 95-3414. Presented at AIAA Flight Simulation Technologies Conference, Baltimore, MD, August 7, 1995.
    [Also available here.]
  25. Jackson, E. Bruce: Manual for a Workstation-based Generic Flight Simulation Program (LaRCsim) Version 1.4. NASA TM-110164, May 1995.
    [Also available here].
  26. Jackson, E. Bruce; Rivers, Robert A.; Chowdhry, Rajiv S.; Ragsdale, W. A.; and Geyer, David W.: Launch Pad Abort of the HL-20 Lifting Body. J. Guidance, Control and Dynamics, vol. 17, no. 6, November-December 1994, pp. 1345-1349.
  27. Rivers, Robert A.; and Jackson, E. Bruce: Preliminary Piloted Simulation Studies of the HL-20 Lifting Body. J. Aircraft, vol. 31, no. 3, May-June 1994.
  28. Jackson, E. Bruce; Rivers, Robert A.; Chowdhry, Rajiv S.; Ragsdale, W. A.; and Geyer, David W.: Launch Pad Abort Capabilities of the HL-20 Lifting Body. NASA TM-4550, May 1994.
  29. Jackson, E. Bruce; Rivers, Robert A.; Chowdhry, Rajiv S.; Ragsdale, W. A.; and Geyer, David W.: Investigation of the Launch Pad Abort Capabilities of the HL-20 Lifting Body. AIAA Paper 93-3690, August 1993.
  30. Jackson, E. Bruce; Rivers, Robert A.; and Bailey, Melvin L.: Effect of Lift-to-Drag Ratio in Pilot Rating of the HL-20 Landing Task. J. Spacecraft and Rockets, vol. 30, no. 5, Sept-Oct 1993, pp. 543-548.
  31. Jackson, E. Bruce; Cruz, Christopher I.; and Ragsdale, W. A.: Real-Time Simulation Model of the HL-20 Lifting Body. NASA TM-107580, July 1992.
    [Simulation model written in C++ for Mac OS X 10.3 is available on request]
  32. Jackson, E. Bruce; and Cruz, Christopher I.: Preliminary Subsonic Aerodynamic Model for Simulation Studies of the HL-20 Lifting Body. NASA TM-4302, 1992.
    [Paper also available here.]
  33. Rivers, Robert A.; Jackson, E. Bruce; and Ragsdale, W. A.: Preliminary Development of the HL-20 Lifting Body Design. Presented at the 35th Symposium of the Society of Experimental Test Pilots, held in Beverly Hills, CA, September 25-28, 1991.
  34. Jackson, E. Bruce; Ragsdale, W. A.; and Powell, Richard W.: Utilization of Simulation Tools in the HL-20 Conceptual Design Process. AIAA Paper No. 91-2955. Presented at the 1991 AIAA Simulation Technology Conference, held in New Orleans, LA, August 18-21, 1991.
  35. Jackson, E. Bruce; Bailey, Melvin L.; and Rivers, Robert A.: Effect of Lift-to-Drag Ratio Upon Pilot Rating for a Preliminary Version of the HL-20 Lifting Body. Presented at the 1991 AIAA Atmospheric Flight Mechanics Conference, held in New Orleans, LA, August 18-21, 1991. AIAA Paper No. 91-2090.
  36. Dowdy, M. C.; Jackson, E. B.; Nichols, J. H.: Controls Analysis and Simulation Test Loop Environment (CASTLE) Programmer's Guide, Version 1.3. Naval Air Test Center Technical Memorandum TM 89-11 SA, 30 March 1989.
  37. Dowdy, M. C.; Jackson, E. B.; Nichols, J. H.; and Sutton, D. D.: Controls Analysis and Simulation Test Loop Environment (CASTLE) User's Guide, Version 1.3. Naval Air Test Center Technical Memorandum TM 89-144 SA, 6 March 1989.
  38. Jackson, E. Bruce; and Coyle, Thomas F.: Assurance of the X-29A Advanced Technology Demonstrator Flight Control Software. AIAA Paper 83-2724, November 1983.
Modified Mon, 05-Oct-2009 by Bruce Jackson (bruce.jackson@nasa.gov)