Comparative analysis of design variants for low altitude flight parameters measuring system
Automatic Control in Aerospace, Volume # 17 | Part# 1
Nebylov, Alexander; Rumyantseva, Elizaveta; Sharan, Sukrit
Digital Object Identifier (DOI)
flight control,low altitude flight,integrated navigation system,motion parameters,digital control,control accuracy
Radio altimeters and inertial sensors integration algorithm synthesis techniques are constructed. Mathematical modeling of integrated system is developed. Synthesis and accuracy analysis task of radio and inertial measuring means integration algorithms is considered for the case of flight near the disturbed sea surface. Integration algorithms synthesis demands system invariance concerning altitude. The structure of the integrated system of motion control with digital implementation is suggested. Principles of different measurement systems and sensors construction are shown. Calculated inertial sensor accuracy allows choosing sensor construction variants. The optimal system parameters are considered.
 Nebylov, A.V. (2004). Ensuring control accuracy. Series: Lecture Notes in Control and Information Sciences. Monograph, Springer, 244 pp.  V.G. Peshekhonov (2003). In: Gyroscopy and navigation on the beginning of XXI century. Gyroscopy and navigation, #4, p. 5-18 (in Russian).  Nebylov, A.V. and P. Wilson (2002). Ekranoplane - Controlled Flight close to Surface. Monograph. WIT-Press, UK, 320 pp.+CD.  Advances in Navigation Sensors and Integration Technology. RTO LECTURE SERIES 232 (2004) PRE-PRINTS. AC/323(SET-064)TP/43.  Nebylov A.V., Rumyantseva E.A. (2005). Accuracy and reliability ensuring for low altitude flight integrated measurement system. IVth International Conference "Aviation and Cosmonautics", Moscow, Russia (in Russian).  Lee S, Park S., Kim J., Yi S. and Cho D. (2000). Surface/Bulk Micromachined Single-crystalline Silicon Micro-gyroscope. In: IEEE/ASME Journal of Microelectromechanical systems, vol. 9, #4, pp. 557- 567.  Stepanov O. A. (2000). Comparative investigation of two nonlinear filters for navigation problems. In: Proceedings of Position, Location and Navigation Symposium, IEEE, San Diego, pp. 333-340.  Nebylov A.V., Rumyantseva E.A., et.al.(2005). Wing-In-Ground Flight Automatic Control System. XVI IFAC Congress, Prague, Proceedings on CD.  Noda A and Sekiguchi T (2001). Status of Micro/Nano Satellite in NASDA. 6th ISU Annual International Symposium, Japan.  Alazard D., Imbert N., Apkarian P. and Clement B (2003). Launcher attitude control: some additional design and optimization tools. In: Proceedings of the 5th International Conference on Launcher Technology, Madrid, pp. 224-230.  Nebylov A.V. (2001). WIG-Flight Automatic Control Principles, Systems and Application Advantages. 15th IFAC Symposium on Automatic Control in Aerospace. Forli, Italy, pp. 542-547.