Design and evaluation of an acceleration guidance algorithm for entry

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2003, Pages

  Saraf, A ^a   Leavitt, J A ^a   Chen, D T ^a   Mease, K D ^a  

^a University of California at Irvine   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DRAG; FEEDBACK LINEARIZATION; TRAJECTORIES;

ACCELERATION GUIDANCE; BANK ANGLE PROFILE; DESIGN AND EVALUATIONS; EXTENSIVE SIMULATIONS; LATERAL ACCELERATION; SPACE TRANSPORTATION VEHICLES; THREE DIMENSIONAL TRAJECTORIES; TRAJECTORY TRACKING;

COMPUTER CIRCUITS;

EID: 85087596385     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5737     Document Type: Conference Paper

References (13)

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3. Hanson, J. M., "Advanced Guidance and Con-trol Project for Reusable Launch Vehicles," Paper Number 2000-3957, AIAA Guidance, Navigation and Control Conference, Denver, 2000.
4. Dukeman, G.A.,"Profile-Following Entry Guid-ance Using Linear Quadratic Regulator Theory," Paper Number 2002-4457, AIAA Guidance, Navigation and Control Conference, Monterey, Aug. 2002.
5. Zimmerman, C., Dukeman, G.A., and Hanson, J.M., "An Automated method to Compute Orbital Re-entry Trajectories with Heating Constraints," Paper Number 2002-4454, AIAA Guidance, Navigation and Control Conference, Monterey, Aug. 2002.
6. Shen, Z. and Lu, P., "Onboard Generation of Three-Dimensional Constrained Entry Trajectories," Journal of Guidance, Control, and Dynamics, Vol. 26, No. 1, 2003, pp. 111-121.
7. Lu, P.,"Entry Guidance and Trajectory Control for Reusable Launch Vehicle," Journal of Guidance, Control and Dynamics, Vol. 20, No. 1, 1997, pp. 143-149.
8. Mease, K.D., Chen, D.T., Teufel, P., and Schönenberger, H., "Reduced-Order Entry Trajectory Planning for Acceleration Guidance," J. Guidance, Control, and Dynam-ics, Vol. 25, No. 2, 2002, pp. 257-266.
9. Stengel, R.F., "Optimal Guidance for the Space Shuttle Transition," J. Spacecraft, Vol. 11, No. 3, 1974, pp. 173-179.
10. Vinh, N.X., Optimal Trajectories in Atmospheric Flight, Elsevier, New York, 1981.
11. Leavitt, J.A., Saraf, A., Chen, D.T. and Mease, K.D., "Performance of Evolved Acceleration Guidance Logic for Entry (EAGLE)," Paper Number 2002-4456, AIAA GNC-Conference, Monterey, Aug. 2002.
12. Saraf, A., Leavitt, J.A., Chen, D.T. and Mease, K.D., "Design and Evalaution of an Acceleration Guidance Al-gorithm for Entry," AIAA Journal of Spacecraft and Rockets, to appear.
13. Hanson, J.M., Coughlin, D.J., Dukeman, G.A., Mulqueen, J.A., and McCarter, J.W., "Ascent, Transition, En-try, and Abort Guidance Algorithm Design for the X-33 Ve-hicle," Paper Number 1998-4409, AIAA Guidance, Navigation and Control Conference, Boston, Aug. 1998.