Оптимизация программы полета дозвукового пассажирского самолета…
9
The way to optimize a flight program of subsonic
passenger aircraft at lowering and braking of the aircraft
by considering operational constraints for civil aviation
© E.A. Gubareva,
T.Yu. Mozzhorina
Bauman Moscow State Technical University, Moscow, 105005, Russia
Flight simulation is based on traditional approaches used for subsonic passenger air-
crafts. Lowering and braking modes of operation are optimized by considering opera-
tional constraints for civil aviation. For simulating flight conditions we used the in-built
model of bypass turbojet engine. It makes possible to calculate power plant parameters
under any flight conditions.
Keywords
: flight simulation, modeling GTE, flight optimization program, passenger air-
craft.
REFERENCES
[1]
Yugov O.K., Selivanov O.D.
Osnovy integratsii samoleta i dvigatelya
[Fundamentals of aircraft and engine integration]. Moscow, Mashinostroenie
Publ., 1989, 304 p.
[2]
Byushgens G.S., ed.
Aerodinamika i dinamika poleta magistralnykh samoletov
[Aerodynamics and flight dynamics of long haul aircraft]. Moscow, TsAGI
Publ., Beijing, PRC Aviaizdatelstvo Publ., 1995, 772 p.
[3]
Shlyakhtenko S.M., ed.
Teoriya dvukhkonturnykh turboreaktivnykh dvigateley
[Theory of bypass turbojet engine]. Moscow, Mashinostroenie Publ., 1979.
[4]
Yankin V.I.
Sistema program dlya rascheta kharakteristik VRD
[The system
of programs for calculating the air-jet engine characteristics]. Moscow,
Mashinostroenie Publ., 1976, 168 p.
[5]
Skripnichenko
S.Yu.Optimizatsiya rezhimov nabora vysoty (ekonomicheskie
rezhimy poleta
) [Optimization of the climb conditions (economic flight
modes)]. Moscow, Mashinostroenie Publ., 1975, 191 p.
[6]
Skripnichenko
S.Yu. Osnovnye napravleniya ekonomichnosti poleta
grazhdanskikh samoletov [Principal directions of civil aircraft economy
flight].
Aviatsiya i kosmonavtika–2003: Tezisy dokl. mezhdunar. nauch. konf.
[International Scientific Conference “Aviation and Cosmonautics’ 2003”.
Abstracts]. Moscow, MAI Publ., 2003, pp. 74–75.
[7]
Skripnichenko
S.Yu. Razvitie energeticheskogo metoda dlya optimizatsii
rezhimov nabora vysoty i snizheniya [The development of the energy method
for optimization of climb and descent].
Sovremennye problemy dinamiki
poleta, aerodinamiki i letnykh ispytaniy. Sbornik dokladov Vserossiyskoy
konferentsii
[Current Problems of Flight Dynamics, Aerodynamics and Flight
Tests. Proceedings of the All-Russian Conference]. Moscow, MAI Publ.,
2004, pp. 110–118.
[8]
Skripnichenko
S.Yu.
Nauchniy Vestnik MGTU GA. Seria Aeromekhanika i
prochnost – Scientific Herald of Moscow State Technical University of Civil
Aviation. Series: Aeromechanics and Strength
, 2005, no. 81, pp. 107–110.
[9]
Kiselev M.A., Kostin A.M., Tyumenev V.R.
Nauchniy Vestnik MGTU GA –
Scientific Herald of Moscow State Technical University of Civil Aviation
,
2008, no. 125, pp. 138–145.