Inverse dynamics approach for real-time determination of feasible aircraft reference trajectories-Reference-Cited by-同舟云学术

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Inverse dynamics approach for real-time determination of feasible aircraft reference trajectories

Published:1999-08-09 Issue: Volume: Page:
ISSN:
Container-title:24th Atmospheric Flight Mechanics Conference
language:
Short-container-title:

Author:

Verma Ajay¹,Junkins John¹

Affiliation:

1. Texas A & M Univ., College Station

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-4241

Reference5 articles.

1. 1991,pp.920-926. 8 Gao,C.,andHess,R.A. "IuverseSimulationof

2. 1993,pp.733-737. 9 Matties,G.,Socio,L., andLeonessa,A. "Solution

3. Dynamics,Vol. 18,No. 3, 1995,pp.567-571. 10 Lee,S.,Kim, Y. "Solutionof theInverse

4. SimulationProblemby OptimizationTechnique andit's Applicationto Aircraft NonlinearLarge AngleManeuvers,"AL4AGuidanceNavigation andControlConference,SanDiego,CA, July29-31,1996.

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