Robust trim procedure for rotorcraft configurations-Reference-Cited by-同舟云学术

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Robust trim procedure for rotorcraft configurations

Published:2015-09 Issue: Volume:45 Page:442-448
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Friedman Chen,Rand Omri

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

1. Helicopter Flight Dynamics, vol. 2;Padfield,2007

2. Helicopter Theory;Johnson,1994

3. Efficient and robust algorithms for trim and stability analysis of advanced rotorcraft simulations;McVicar;Aeronaut. J.,1997

4. Helicopter trim by periodic shooting with Newton–Raphson iteration;Peters,1981

5. Helicopter trim analysis by shooting and finite element methods with optimally damped Newton iterations;Achar;AIAA J.,1993

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1. Some improvements of hybrid trim method for a helicopter rotor in forward flight;Aerospace Science and Technology;2021-06

2. A study of coaxial rotor aerodynamic interaction mechanism in hover with high-efficient trim model;Aerospace Science and Technology;2019-01

3. A port-Hamiltonian framework for operator force assisting systems: Application to the design of helicopter flight controls;Aerospace Science and Technology;2018-01

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