| 參考文獻 |
[1] Connor, M. A.,"Optimization of a Lateral Turn at Constant Height,"
AIAA Journal, Vol.~5, No.~2, Feb.~1967, pp.~335--338.
[2] Bryson, A. E. and Lele, M. L."Minimum Fuel Lateral Turns at Constant
Altitude,"AIAA Journal, Vol.~7, No.~3 March 1969, pp.~559--560.
[3] Hedrick, J. K. and Bryson, A. E. Jr.,"Three-Dimensional,
Minimum Fuel Turns for a Supersonic Aircraft,"Journal of Aircraft,
Vol.~9, No.~3, March 1972, pp.~223--229.
[4] Vinh, N. X.,"Minimum Fuel Rocket Maneuvers in Horizontal Flight,"
AIAA Journal, Vol.~11, No.~2, Feb.~1973, pp.~165--169.
[5] Vinh, N. X.,Optimal Trajectory in Atmospherical Flight,
Elevier Scientific, Amsterdam, 1981.
[6] Burrows, J. W.,"Fuel Optimal Trajectory Computation,"
Journal of Aircraft, Vol.~19, No.~4, Apr.~1982, pp.~324--329.
[7] Kreindler, E. and Neuman, F.,
"Minimum Fuel Horizontal Flight Paths in the Terminal Area,"
Journal of Guidance and Control,
Vol.~5, No.~5, Sept.--Oct. 1982, pp.~490--497.
[8] Burrows, J. W.,"Fuel-Optimal Aircraft Trajectories with Fixed
Arrival Times,"Journal of Guidance and Control,
Vol.~6, No.~1, Jan.--Feb. 1983, pp.~14--19.
[9] Neuman, F.,"Minimum-Fuel, Three-Dimensional Flight Paths for Jet
Transport,"Journal of Guidance and Control,
Vol.~8, No.~5, Sept.--Oct. 1985, pp.~650--657.
[10] Sorensen, J. A. and Waters, M. H.,
"Airborne Method to Minimum Fuel with Fixed Time-of-Arrival
Constraints,"Journal of Guidance and Control,
Vol.~4, No.~3, May--June 1981, pp.~348--349.
[11] Bryson, A. E., Jr., and Ho, Y.C.,
Applied Optimal Control, Hemisphere Publishing Co.,
New York, U.S.A., 1975.
[12] Bousson, K.,"Single Gridpoint Dynamic Programming for
Trajectory Optimization,"AIAA-2005-5902,
AIAA Atmospheric Flight Mechanics
Conference and Exhibit, San Francisco, California, Aug. 15-18,2005
[13] Bertsekas, D. P.,
Dynamic Programming and Optimal Control, Vol. I,
Athena Scientific, Belmont, MA, U.S.A., 2000.
[14] U.S. Standard Atmosphere, 1976,
National Oceanic and Atmospheric Administration, NASA,
U.S. Air Force, Washington, DC, U.S.A., 1976.
[15] Bryson, A. E., Jr., Desai, M. N., and Hoffman, W. C.,
"Energy-State Approximation in Performance Optimization
of Supersonic Aircraft,"Journal of Aircraft,
Vol.~6, No.~6, November--December 1969, pp.~481--488.
|
