Procedural Guide For Modeling And Analyzing The Flight Dynamics Of The SH-60B Helicopter Using Flightlab - Info and Reading Options
By Wagner, Roy C.
"Procedural Guide For Modeling And Analyzing The Flight Dynamics Of The SH-60B Helicopter Using Flightlab" and the language of the book is English.
“Procedural Guide For Modeling And Analyzing The Flight Dynamics Of The SH-60B Helicopter Using Flightlab” Metadata:
- Title: ➤ Procedural Guide For Modeling And Analyzing The Flight Dynamics Of The SH-60B Helicopter Using Flightlab
- Author: Wagner, Roy C.
- Language: English
Edition Identifiers:
- Internet Archive ID: proceduralguidef109457596
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"Procedural Guide For Modeling And Analyzing The Flight Dynamics Of The SH-60B Helicopter Using Flightlab" Description:
The Internet Archive:
This thesis uses Flightlab to model and analyze the flight dynamics of the SH-6OB Seahawk helicopter. Flightlab runs on computers utilizing the UNIX operating system and is used for design, analysis and testing of an aircraft using non-linear modeling techniques. It is capable of modeling conventional main rotor-tail rotor and tandem rotor helicopters and tilt rotor aircraft. A procedural guide for modeling and analyzing a single main rotor helicopter is presented using the SH-60B. The non-linear response from lateral and longitudinal cyclic, main rotor collective and tail rotor collective inputs are presented. Flightlab is also capable of reducing the non-linear model to a linear model. The linear and non-linear models are then compared. The purpose of this thesis is to present a guide for using Flightlab to model and analyze an existing helicopter design, and also to have in place a well tested model to be used for further research.
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