According to the test results, in order to ensure quality, facilitate production, and
improve efficiency, the flow symmetry index of steering gear is improved.
(3) Conclusion
After taking the above improvement measures, the production of gas steering
engine is relatively smooth, the previous faults do not recur, the routine ignition test
passes once, and the quality of product is no longer affected by the unreliable
quality of gas steering engine. Practice shows that these improvement measures are
effective.
Bibliography
1. Yin Y, Zhang L, Gao Z et al (2012) Analysis of attitude control method of flight machine
based on gas-jet side force. In: Proceedings of the 2011 international conference on advances
in construction machinery and vehicle engineering, Chinese construction machinery society,
Shanghai Scientific & Technical Publishers, pp 413–418
2. Yin Y (2012) Electro-hydraulic servo control theory and application technology in extreme
environment. Shanghai science and technology press, Shanghai
3. Zhang L (2012) Research on attitude control system of aerocraft based on jet reaction force
(0920030068). Tongji university master’s thesis
4. Song J (1996) Use gas generator and nozzle to generate lateral force to change the direction of
the missile. Autoplot Infrared Technol 3:47–48
5. Qu X (1996) Technology of gas rudder and steering gear. Autoplot Infrared Technol 3:51–55
6. Wu H (1982) Structure and strength calculation of turbine parts. China machine press, Beijing
7. Robeson RE (1980) Space vehicle attitude control technology for 20 years. Foreign Space
Technol 2:48–57
8. Deng Y, Tian J, Wang Y et al (2006) Overview of aerocraft attitude control methods. Tactical
Missile Control Technol 02:7–13
9. Wang X-R, Zhou C-S, Ju Y-T, Jiang G-Z (2008) Counter design for length-shorted nozzle of
solid rocket engine. J Ballist 20(4):77–80
10. Chen W-M, Huang S-B, He Y-J (2009) Study on reaction-jet controller of air-to-air missile.
Aero Weapon 2:43–46
11. Kurtenbach FJ (1981) Flight evaluation of a simplified gross thrust calculation technique
using an F100 turbofan engine in an F-15 airplane. NASA Technical Paper 1782
12. Kurtenbach FJ (1979) Evaluation of a simplified gross thrust calculation technique using two
prototype F100 turbofan engines in an altitude facility. NASA TP 1482
13. Hughes DL (1981) Comparison of three thrust calculation methods using in-flight thrust data.
NASA Technical Memorandum 81360
14. Biesradny Thomas J, Lee D, Rodriguez Jose R (1978) Airflow and thrust calibration of an
F100 engine S/N P68005 at selected flight condition. NASA TP 21069
15. Chen Z (2004) Engineering fluid mechanics. Higher Education Press, Beijing
194
10 Application of Aerodynamic Technology in Attitude Control …
improve efficiency, the flow symmetry index of steering gear is improved.
(3) Conclusion
After taking the above improvement measures, the production of gas steering
engine is relatively smooth, the previous faults do not recur, the routine ignition test
passes once, and the quality of product is no longer affected by the unreliable
quality of gas steering engine. Practice shows that these improvement measures are
effective.
Bibliography
1. Yin Y, Zhang L, Gao Z et al (2012) Analysis of attitude control method of flight machine
based on gas-jet side force. In: Proceedings of the 2011 international conference on advances
in construction machinery and vehicle engineering, Chinese construction machinery society,
Shanghai Scientific & Technical Publishers, pp 413–418
2. Yin Y (2012) Electro-hydraulic servo control theory and application technology in extreme
environment. Shanghai science and technology press, Shanghai
3. Zhang L (2012) Research on attitude control system of aerocraft based on jet reaction force
(0920030068). Tongji university master’s thesis
4. Song J (1996) Use gas generator and nozzle to generate lateral force to change the direction of
the missile. Autoplot Infrared Technol 3:47–48
5. Qu X (1996) Technology of gas rudder and steering gear. Autoplot Infrared Technol 3:51–55
6. Wu H (1982) Structure and strength calculation of turbine parts. China machine press, Beijing
7. Robeson RE (1980) Space vehicle attitude control technology for 20 years. Foreign Space
Technol 2:48–57
8. Deng Y, Tian J, Wang Y et al (2006) Overview of aerocraft attitude control methods. Tactical
Missile Control Technol 02:7–13
9. Wang X-R, Zhou C-S, Ju Y-T, Jiang G-Z (2008) Counter design for length-shorted nozzle of
solid rocket engine. J Ballist 20(4):77–80
10. Chen W-M, Huang S-B, He Y-J (2009) Study on reaction-jet controller of air-to-air missile.
Aero Weapon 2:43–46
11. Kurtenbach FJ (1981) Flight evaluation of a simplified gross thrust calculation technique
using an F100 turbofan engine in an F-15 airplane. NASA Technical Paper 1782
12. Kurtenbach FJ (1979) Evaluation of a simplified gross thrust calculation technique using two
prototype F100 turbofan engines in an altitude facility. NASA TP 1482
13. Hughes DL (1981) Comparison of three thrust calculation methods using in-flight thrust data.
NASA Technical Memorandum 81360
14. Biesradny Thomas J, Lee D, Rodriguez Jose R (1978) Airflow and thrust calibration of an
F100 engine S/N P68005 at selected flight condition. NASA TP 21069
15. Chen Z (2004) Engineering fluid mechanics. Higher Education Press, Beijing
194
10 Application of Aerodynamic Technology in Attitude Control …