Closed-loop atmospheric ascent guidance based on finite element method

Author： Lu Baogang Cui Naigang Fu Yu Shan Wenzhao Chang Xiaohua

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.87, Iss.5, 2015-09, pp. : 393-401

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Use of Rotor State Feedback to Improve Closed-Loop Stability and Handling Qualities

By Horn Joseph F. Guo Wei Ozdemir Gurbuz Taha

Journal of the American Helicopter Society, Vol. 57, Iss. 2, 2012-04 ,pp. : 1-10

AHS International

Access to resources Recommend Favorite

Application of the Finite Element Method to Rotary-Wing Aeroelasticity

By Friedmann P. P. Straub F.

Journal of the American Helicopter Society, Vol. 25, Iss. 1, 1980-01 ,pp. : 36-44

AHS International

Access to resources Recommend Favorite

A Numerical Simulation Study of Open-Loop, Closed-Loop and Adaptive Multicyclic Control Systems

By Chopra Inderjit McCloud John L.

Journal of the American Helicopter Society, Vol. 28, Iss. 1, 1983-01 ,pp. : 63-77

AHS International

Access to resources Recommend Favorite

Transmission Design Using Finite Element Method Analysis Techniques

By Albrecht Carl

Journal of the American Helicopter Society, Vol. 33, Iss. 2, 1988-04 ,pp. : 3-14

AHS International

Access to resources Recommend Favorite

A General Method for Modifying a Finite-Element Model to Correlate with Modal Test Data

By Twomey William J. Chen Timothy L. C. Ojalvo Irving U. Ting Tienko

Journal of the American Helicopter Society, Vol. 36, Iss. 3, 1991-07 ,pp. : 48-58

AHS International

Access to resources Recommend Favorite