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You searched for subject:( Handling qualities). Showing records 1 – 26 of 26 total matches.

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Penn State University

1. Conti, Angelina Maria. Incorporating Handling Qualities Assessment into the Design of Compound Rotorcraft.

Degree: 2018, Penn State University

 The next fleet of rotorcraft will need to achieve higher forward flight speeds to meet the demanding requirements of military operation. One potential solution is… (more)

Subjects/Keywords: Flight Controls; Helicopters; Rotorcraft; ADS-33; Flight Handling Qualities

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Conti, A. M. (2018). Incorporating Handling Qualities Assessment into the Design of Compound Rotorcraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/15143aic5390

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Conti, Angelina Maria. “Incorporating Handling Qualities Assessment into the Design of Compound Rotorcraft.” 2018. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/15143aic5390.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Conti, Angelina Maria. “Incorporating Handling Qualities Assessment into the Design of Compound Rotorcraft.” 2018. Web. 24 Jan 2021.

Vancouver:

Conti AM. Incorporating Handling Qualities Assessment into the Design of Compound Rotorcraft. [Internet] [Thesis]. Penn State University; 2018. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/15143aic5390.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Conti AM. Incorporating Handling Qualities Assessment into the Design of Compound Rotorcraft. [Thesis]. Penn State University; 2018. Available from: https://submit-etda.libraries.psu.edu/catalog/15143aic5390

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Penn State University

2. Berger, Tom. Handling Qualities Requirements and Control Design for High-Speed Rotorcraft.

Degree: 2019, Penn State University

 The U.S. Department of Defense has established the Future Vertical Lift initiative to develop a family of next-generation vertical lift aircraft that will fly farther,… (more)

Subjects/Keywords: Rotorcraft; Handling Qualities; Flight Control System; Control Laws; Tiltrotor; Compound Helicopter

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APA (6th Edition):

Berger, T. (2019). Handling Qualities Requirements and Control Design for High-Speed Rotorcraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/17211tub246

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Berger, Tom. “Handling Qualities Requirements and Control Design for High-Speed Rotorcraft.” 2019. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/17211tub246.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Berger, Tom. “Handling Qualities Requirements and Control Design for High-Speed Rotorcraft.” 2019. Web. 24 Jan 2021.

Vancouver:

Berger T. Handling Qualities Requirements and Control Design for High-Speed Rotorcraft. [Internet] [Thesis]. Penn State University; 2019. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/17211tub246.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Berger T. Handling Qualities Requirements and Control Design for High-Speed Rotorcraft. [Thesis]. Penn State University; 2019. Available from: https://submit-etda.libraries.psu.edu/catalog/17211tub246

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Penn State University

3. ONeill, Eric Paul. MODELING AND CONTROL OF TRAILING EDGE FLAPS FOR GUST ALLEVIATION AND HANDLING QUALITIES .

Degree: 2011, Penn State University

 Operating a helicopter in a turbulent wind environment is a difficult challenge for a pilot. Tasks that would be simple in a calm environment become… (more)

Subjects/Keywords: SH-2G; UH-60; Trailing Edge Flaps; Handling Qualities

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APA (6th Edition):

ONeill, E. P. (2011). MODELING AND CONTROL OF TRAILING EDGE FLAPS FOR GUST ALLEVIATION AND HANDLING QUALITIES . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/12646

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

ONeill, Eric Paul. “MODELING AND CONTROL OF TRAILING EDGE FLAPS FOR GUST ALLEVIATION AND HANDLING QUALITIES .” 2011. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/12646.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

ONeill, Eric Paul. “MODELING AND CONTROL OF TRAILING EDGE FLAPS FOR GUST ALLEVIATION AND HANDLING QUALITIES .” 2011. Web. 24 Jan 2021.

Vancouver:

ONeill EP. MODELING AND CONTROL OF TRAILING EDGE FLAPS FOR GUST ALLEVIATION AND HANDLING QUALITIES . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/12646.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

ONeill EP. MODELING AND CONTROL OF TRAILING EDGE FLAPS FOR GUST ALLEVIATION AND HANDLING QUALITIES . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/12646

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Toronto

4. Peterson, Timothy Shaw. Handling Qualities of a Blended Wing Body Aircraft.

Degree: 2011, University of Toronto

The blended wing body (BWB) is a tailless aircraft with the potential to use 27% less fuel than a conventional aircraft with the same passenger… (more)

Subjects/Keywords: flight simulation; handling qualities; blended wing body; 0538

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APA (6th Edition):

Peterson, T. S. (2011). Handling Qualities of a Blended Wing Body Aircraft. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/31384

Chicago Manual of Style (16th Edition):

Peterson, Timothy Shaw. “Handling Qualities of a Blended Wing Body Aircraft.” 2011. Masters Thesis, University of Toronto. Accessed January 24, 2021. http://hdl.handle.net/1807/31384.

MLA Handbook (7th Edition):

Peterson, Timothy Shaw. “Handling Qualities of a Blended Wing Body Aircraft.” 2011. Web. 24 Jan 2021.

Vancouver:

Peterson TS. Handling Qualities of a Blended Wing Body Aircraft. [Internet] [Masters thesis]. University of Toronto; 2011. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1807/31384.

Council of Science Editors:

Peterson TS. Handling Qualities of a Blended Wing Body Aircraft. [Masters Thesis]. University of Toronto; 2011. Available from: http://hdl.handle.net/1807/31384


Delft University of Technology

5. Damveld, H.J. A Cybernetic Approach to Assess the Longitudinal Handling Qualities of Aeroelastic Aircraft.

Degree: 2009, Delft University of Technology

 The future demand for larger and lighter civil transport aircraft leads to more flexible aircraft, which bring their own controlling and handling problems. A review… (more)

Subjects/Keywords: Handling Qualities; Aeroelasticity; Cybernetics

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APA (6th Edition):

Damveld, H. J. (2009). A Cybernetic Approach to Assess the Longitudinal Handling Qualities of Aeroelastic Aircraft. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab

Chicago Manual of Style (16th Edition):

Damveld, H J. “A Cybernetic Approach to Assess the Longitudinal Handling Qualities of Aeroelastic Aircraft.” 2009. Doctoral Dissertation, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab.

MLA Handbook (7th Edition):

Damveld, H J. “A Cybernetic Approach to Assess the Longitudinal Handling Qualities of Aeroelastic Aircraft.” 2009. Web. 24 Jan 2021.

Vancouver:

Damveld HJ. A Cybernetic Approach to Assess the Longitudinal Handling Qualities of Aeroelastic Aircraft. [Internet] [Doctoral dissertation]. Delft University of Technology; 2009. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab.

Council of Science Editors:

Damveld HJ. A Cybernetic Approach to Assess the Longitudinal Handling Qualities of Aeroelastic Aircraft. [Doctoral Dissertation]. Delft University of Technology; 2009. Available from: http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; urn:NBN:nl:ui:24-uuid:3869d074-4e3c-4738-b445-15dbdfd51cab ; http://resolver.tudelft.nl/uuid:3869d074-4e3c-4738-b445-15dbdfd51cab


Delft University of Technology

6. van Bruchem, Barend-Jan (author). Helicopter drive train modelling for manoeuvre load alleviation.

Degree: 2017, Delft University of Technology

 Helicopters are complex and expensive aircraft with a level of technology that is immature compared to fixed- wing counterparts. Helicopters suffer from vibratory loads stemming… (more)

Subjects/Keywords: UH-60; TRDT; Handling Qualities; Structural Load Alleviation; Modelling

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APA (6th Edition):

van Bruchem, B. (. (2017). Helicopter drive train modelling for manoeuvre load alleviation. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:433d35fd-0475-4863-90dc-4ed2a6d34b70

Chicago Manual of Style (16th Edition):

van Bruchem, Barend-Jan (author). “Helicopter drive train modelling for manoeuvre load alleviation.” 2017. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:433d35fd-0475-4863-90dc-4ed2a6d34b70.

MLA Handbook (7th Edition):

van Bruchem, Barend-Jan (author). “Helicopter drive train modelling for manoeuvre load alleviation.” 2017. Web. 24 Jan 2021.

Vancouver:

van Bruchem B(. Helicopter drive train modelling for manoeuvre load alleviation. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:433d35fd-0475-4863-90dc-4ed2a6d34b70.

Council of Science Editors:

van Bruchem B(. Helicopter drive train modelling for manoeuvre load alleviation. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:433d35fd-0475-4863-90dc-4ed2a6d34b70


Penn State University

7. Soneson, Gregory Lorentz. Development and Piloted Simulation Testing of Advanced Response Types for Ship-based Rotorcraft.

Degree: 2014, Penn State University

 Piloted simulation tests were conducted to develop and evaluate advanced control laws and optimal response types for ship-based rotorcraft. Simulations used the GENHEL-PSU non-linear flight… (more)

Subjects/Keywords: Helicopter; Rotorcraft; Controls; Simulation; Handling Qualities; Shipboard; Response Types; Non-Linear Dynamic Inversion

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APA (6th Edition):

Soneson, G. L. (2014). Development and Piloted Simulation Testing of Advanced Response Types for Ship-based Rotorcraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/22764

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Soneson, Gregory Lorentz. “Development and Piloted Simulation Testing of Advanced Response Types for Ship-based Rotorcraft.” 2014. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/22764.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Soneson, Gregory Lorentz. “Development and Piloted Simulation Testing of Advanced Response Types for Ship-based Rotorcraft.” 2014. Web. 24 Jan 2021.

Vancouver:

Soneson GL. Development and Piloted Simulation Testing of Advanced Response Types for Ship-based Rotorcraft. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/22764.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Soneson GL. Development and Piloted Simulation Testing of Advanced Response Types for Ship-based Rotorcraft. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/22764

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Penn State University

8. Zheng, Albert. Investigation of Bandwidth and Disturbance Rejection Properties of a Dynamic Inversion Control Law for Ship-Based Rotorcraft.

Degree: 2015, Penn State University

 This thesis is an investigation to better understand the bandwidth and the disturbance rejection requirements of a non-linear dynamic inversion (NLDI) controller (and for rotorcraft… (more)

Subjects/Keywords: Helicopter; Rotorcraft; Flight Controls; Simulation; Handling Qualities; Shipboard; Bandwidth; Disturbance Rejection; Pilot

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APA (6th Edition):

Zheng, A. (2015). Investigation of Bandwidth and Disturbance Rejection Properties of a Dynamic Inversion Control Law for Ship-Based Rotorcraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/27468

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Zheng, Albert. “Investigation of Bandwidth and Disturbance Rejection Properties of a Dynamic Inversion Control Law for Ship-Based Rotorcraft.” 2015. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/27468.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Zheng, Albert. “Investigation of Bandwidth and Disturbance Rejection Properties of a Dynamic Inversion Control Law for Ship-Based Rotorcraft.” 2015. Web. 24 Jan 2021.

Vancouver:

Zheng A. Investigation of Bandwidth and Disturbance Rejection Properties of a Dynamic Inversion Control Law for Ship-Based Rotorcraft. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/27468.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Zheng A. Investigation of Bandwidth and Disturbance Rejection Properties of a Dynamic Inversion Control Law for Ship-Based Rotorcraft. [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/27468

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Delft University of Technology

9. van Lierop, Bas (author). Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft.

Degree: 2017, Delft University of Technology

 With the introduction of the BS115, an ultra-light two-seater general aviation aircraft, a new opportunity for military pilot training is presented. To increase the training… (more)

Subjects/Keywords: General Aviation; Handling Qualities; Training Effectiveness; Military; Pilot training; flight testing; DATCOM

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APA (6th Edition):

van Lierop, B. (. (2017). Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:33534a03-6d57-4175-9c3e-116b9e8fe3ea

Chicago Manual of Style (16th Edition):

van Lierop, Bas (author). “Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft.” 2017. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:33534a03-6d57-4175-9c3e-116b9e8fe3ea.

MLA Handbook (7th Edition):

van Lierop, Bas (author). “Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft.” 2017. Web. 24 Jan 2021.

Vancouver:

van Lierop B(. Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:33534a03-6d57-4175-9c3e-116b9e8fe3ea.

Council of Science Editors:

van Lierop B(. Handling Qualities Criteria for Training Effectiveness Assessment of the BS115 Aircraft. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:33534a03-6d57-4175-9c3e-116b9e8fe3ea


Penn State University

10. Yomchinda, Thanan. Integrated Flight Control Design and Handling Qualities Analysis for a Tiltrotor Aircraft.

Degree: 2009, Penn State University

 Tiltrotor aircraft present a challenge for flight control designers and handling qualities engineers. Achieving consistent handling qualities throughout an operational flight envelope is difficult since… (more)

Subjects/Keywords: Model Inversion Control Law; Flight Control; Aircraft Handling Qualities

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APA (6th Edition):

Yomchinda, T. (2009). Integrated Flight Control Design and Handling Qualities Analysis for a Tiltrotor Aircraft. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/9130

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Yomchinda, Thanan. “Integrated Flight Control Design and Handling Qualities Analysis for a Tiltrotor Aircraft.” 2009. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/9130.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Yomchinda, Thanan. “Integrated Flight Control Design and Handling Qualities Analysis for a Tiltrotor Aircraft.” 2009. Web. 24 Jan 2021.

Vancouver:

Yomchinda T. Integrated Flight Control Design and Handling Qualities Analysis for a Tiltrotor Aircraft. [Internet] [Thesis]. Penn State University; 2009. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/9130.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Yomchinda T. Integrated Flight Control Design and Handling Qualities Analysis for a Tiltrotor Aircraft. [Thesis]. Penn State University; 2009. Available from: https://submit-etda.libraries.psu.edu/catalog/9130

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Delft University of Technology

11. Sluiter, Carlijn (author). Bicycle Handling Qualities: finding objective measures for subjective handling qualities.

Degree: 2018, Delft University of Technology

Subjects/Keywords: Bicycle; Handling Qualities; Subjective; Objective measure; Correlations

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Sluiter, C. (. (2018). Bicycle Handling Qualities: finding objective measures for subjective handling qualities. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d8f74cbd-0326-4908-8e84-0b85d9d80a0b

Chicago Manual of Style (16th Edition):

Sluiter, Carlijn (author). “Bicycle Handling Qualities: finding objective measures for subjective handling qualities.” 2018. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:d8f74cbd-0326-4908-8e84-0b85d9d80a0b.

MLA Handbook (7th Edition):

Sluiter, Carlijn (author). “Bicycle Handling Qualities: finding objective measures for subjective handling qualities.” 2018. Web. 24 Jan 2021.

Vancouver:

Sluiter C(. Bicycle Handling Qualities: finding objective measures for subjective handling qualities. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:d8f74cbd-0326-4908-8e84-0b85d9d80a0b.

Council of Science Editors:

Sluiter C(. Bicycle Handling Qualities: finding objective measures for subjective handling qualities. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:d8f74cbd-0326-4908-8e84-0b85d9d80a0b


Cranfield University

12. Guo, Wei. Gain scheduling for a passenger aircraft control system to satisfy handling qualities.

Degree: MSc by Research, 2010, Cranfield University

 This thesis considers the problem of designing gain scheduled flight control system (FCS) for large transport aircraft that satisfy handling qualities criteria. The goal is… (more)

Subjects/Keywords: Gain Scheduling; Flight Control System; Handling Qualities; Rate Command-Attitude Hold; Passenger Aircraft; Flight Dynamics; Boeing 747

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APA (6th Edition):

Guo, W. (2010). Gain scheduling for a passenger aircraft control system to satisfy handling qualities. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/6701

Chicago Manual of Style (16th Edition):

Guo, Wei. “Gain scheduling for a passenger aircraft control system to satisfy handling qualities.” 2010. Masters Thesis, Cranfield University. Accessed January 24, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/6701.

MLA Handbook (7th Edition):

Guo, Wei. “Gain scheduling for a passenger aircraft control system to satisfy handling qualities.” 2010. Web. 24 Jan 2021.

Vancouver:

Guo W. Gain scheduling for a passenger aircraft control system to satisfy handling qualities. [Internet] [Masters thesis]. Cranfield University; 2010. [cited 2021 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/6701.

Council of Science Editors:

Guo W. Gain scheduling for a passenger aircraft control system to satisfy handling qualities. [Masters Thesis]. Cranfield University; 2010. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/6701


Cranfield University

13. Andrews, Stuart P. Modelling and simulation of flexible aircraft : handling qualities with active load control.

Degree: PhD, 2011, Cranfield University

 The study of the motion of manoeuvring aircraft has traditionally considered the aircraft to be rigid. This simplifying assumption has been shown to give quite… (more)

Subjects/Keywords: Flexible; Elastic; Civil Transport; Aeroplane; Flight Dynamics; Handling Qualities; Aeroelasticity; Aeroservoelasticity; Structural Dynamics; Unsteady Aerodynamics; Load Alleviation

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APA (6th Edition):

Andrews, S. P. (2011). Modelling and simulation of flexible aircraft : handling qualities with active load control. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7705

Chicago Manual of Style (16th Edition):

Andrews, Stuart P. “Modelling and simulation of flexible aircraft : handling qualities with active load control.” 2011. Doctoral Dissertation, Cranfield University. Accessed January 24, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/7705.

MLA Handbook (7th Edition):

Andrews, Stuart P. “Modelling and simulation of flexible aircraft : handling qualities with active load control.” 2011. Web. 24 Jan 2021.

Vancouver:

Andrews SP. Modelling and simulation of flexible aircraft : handling qualities with active load control. [Internet] [Doctoral dissertation]. Cranfield University; 2011. [cited 2021 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7705.

Council of Science Editors:

Andrews SP. Modelling and simulation of flexible aircraft : handling qualities with active load control. [Doctoral Dissertation]. Cranfield University; 2011. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7705


Cranfield University

14. Andrews, Stuart P. Modelling and simulation of flexible aircraft : handling qualities with active load control.

Degree: PhD, 2011, Cranfield University

 The study of the motion of manoeuvring aircraft has traditionally considered the aircraft to be rigid. This simplifying assumption has been shown to give quite… (more)

Subjects/Keywords: Flexible; Elastic; Civil Transport; Aeroplane; Flight Dynamics; Handling Qualities; Aeroelasticity; Aeroservoelasticity; Structural Dynamics; Unsteady Aerodynamics; Load Alleviation

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APA (6th Edition):

Andrews, S. P. (2011). Modelling and simulation of flexible aircraft : handling qualities with active load control. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/7705 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566018

Chicago Manual of Style (16th Edition):

Andrews, Stuart P. “Modelling and simulation of flexible aircraft : handling qualities with active load control.” 2011. Doctoral Dissertation, Cranfield University. Accessed January 24, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/7705 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566018.

MLA Handbook (7th Edition):

Andrews, Stuart P. “Modelling and simulation of flexible aircraft : handling qualities with active load control.” 2011. Web. 24 Jan 2021.

Vancouver:

Andrews SP. Modelling and simulation of flexible aircraft : handling qualities with active load control. [Internet] [Doctoral dissertation]. Cranfield University; 2011. [cited 2021 Jan 24]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7705 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566018.

Council of Science Editors:

Andrews SP. Modelling and simulation of flexible aircraft : handling qualities with active load control. [Doctoral Dissertation]. Cranfield University; 2011. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/7705 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.566018


Penn State University

15. Spires, James Michael. MODEL FOLLOWING AND HIGH ORDER AUGMENTATION FOR ROTORCRAFT CONTROL, APPLIED VIA PARTIAL AUTHORITY.

Degree: 2017, Penn State University

 This dissertation consists of two main studies, a few small studies, and design documentation, all aimed at improving rotorcraft control by employing multi-input multi-output (MIMO)… (more)

Subjects/Keywords: rotorcraft control; model following control; dynamic decoupling; explicit model following; H2; Hinf; dynamic inversion; nonlinear dynamic inversion; handling qualities; partial authority control; feed forward; turbulence rejection; piggyback compensation

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APA (6th Edition):

Spires, J. M. (2017). MODEL FOLLOWING AND HIGH ORDER AUGMENTATION FOR ROTORCRAFT CONTROL, APPLIED VIA PARTIAL AUTHORITY. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13773jms1188

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Spires, James Michael. “MODEL FOLLOWING AND HIGH ORDER AUGMENTATION FOR ROTORCRAFT CONTROL, APPLIED VIA PARTIAL AUTHORITY.” 2017. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/13773jms1188.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Spires, James Michael. “MODEL FOLLOWING AND HIGH ORDER AUGMENTATION FOR ROTORCRAFT CONTROL, APPLIED VIA PARTIAL AUTHORITY.” 2017. Web. 24 Jan 2021.

Vancouver:

Spires JM. MODEL FOLLOWING AND HIGH ORDER AUGMENTATION FOR ROTORCRAFT CONTROL, APPLIED VIA PARTIAL AUTHORITY. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/13773jms1188.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Spires JM. MODEL FOLLOWING AND HIGH ORDER AUGMENTATION FOR ROTORCRAFT CONTROL, APPLIED VIA PARTIAL AUTHORITY. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/13773jms1188

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

16. Antonioli, Jean-Charles. Spécification de lois de commande pour hélicoptères orientée Qualités de Vol : Designing helicopter control laws with Handling Qualities objectives.

Degree: Docteur es, Automatique, 2015, Aix Marseille Université

Cette thèse s'inscrit dans le domaine de l’étude des lois de commandes de vol pour hélicoptères. Les automaticiens doivent régler les gains de ces lois… (more)

Subjects/Keywords: Critères de Qualités de Vol; Norme ADS-33; Hélicoptère; Automatique classique; Commande; Pid; Handling Qualities requirements; ADS-33 standard; Helicopter; Automatics; Control; Pid

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APA (6th Edition):

Antonioli, J. (2015). Spécification de lois de commande pour hélicoptères orientée Qualités de Vol : Designing helicopter control laws with Handling Qualities objectives. (Doctoral Dissertation). Aix Marseille Université. Retrieved from http://www.theses.fr/2015AIXM4333

Chicago Manual of Style (16th Edition):

Antonioli, Jean-Charles. “Spécification de lois de commande pour hélicoptères orientée Qualités de Vol : Designing helicopter control laws with Handling Qualities objectives.” 2015. Doctoral Dissertation, Aix Marseille Université. Accessed January 24, 2021. http://www.theses.fr/2015AIXM4333.

MLA Handbook (7th Edition):

Antonioli, Jean-Charles. “Spécification de lois de commande pour hélicoptères orientée Qualités de Vol : Designing helicopter control laws with Handling Qualities objectives.” 2015. Web. 24 Jan 2021.

Vancouver:

Antonioli J. Spécification de lois de commande pour hélicoptères orientée Qualités de Vol : Designing helicopter control laws with Handling Qualities objectives. [Internet] [Doctoral dissertation]. Aix Marseille Université 2015. [cited 2021 Jan 24]. Available from: http://www.theses.fr/2015AIXM4333.

Council of Science Editors:

Antonioli J. Spécification de lois de commande pour hélicoptères orientée Qualités de Vol : Designing helicopter control laws with Handling Qualities objectives. [Doctoral Dissertation]. Aix Marseille Université 2015. Available from: http://www.theses.fr/2015AIXM4333

17. Denieul, Yann. Conception préliminaire de surfaces de contrôle et lois de commande pour configurations d’avions non conventionnelles : Preliminary Design of Control Surfaces and Laws for Unconventional Aircraft Configurations.

Degree: Docteur es, Automatique, 2016, Toulouse, ISAE

La prochaine génération d’avions civil sera probablement une révolution en termede configuration d’avion, différant largement de l’architecture désormais classique “fuselage- ailes- moteurs sous voilure”. Du… (more)

Subjects/Keywords: Dimensionnement avion; Systèmes commandes de vol; Lois de commande; Optimisation; Qualités de vol; Aircraft Design; Flight Control Systems; Control Laws; Optimization; Handling Qualities; 629.8

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APA (6th Edition):

Denieul, Y. (2016). Conception préliminaire de surfaces de contrôle et lois de commande pour configurations d’avions non conventionnelles : Preliminary Design of Control Surfaces and Laws for Unconventional Aircraft Configurations. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2016ESAE0033

Chicago Manual of Style (16th Edition):

Denieul, Yann. “Conception préliminaire de surfaces de contrôle et lois de commande pour configurations d’avions non conventionnelles : Preliminary Design of Control Surfaces and Laws for Unconventional Aircraft Configurations.” 2016. Doctoral Dissertation, Toulouse, ISAE. Accessed January 24, 2021. http://www.theses.fr/2016ESAE0033.

MLA Handbook (7th Edition):

Denieul, Yann. “Conception préliminaire de surfaces de contrôle et lois de commande pour configurations d’avions non conventionnelles : Preliminary Design of Control Surfaces and Laws for Unconventional Aircraft Configurations.” 2016. Web. 24 Jan 2021.

Vancouver:

Denieul Y. Conception préliminaire de surfaces de contrôle et lois de commande pour configurations d’avions non conventionnelles : Preliminary Design of Control Surfaces and Laws for Unconventional Aircraft Configurations. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2016. [cited 2021 Jan 24]. Available from: http://www.theses.fr/2016ESAE0033.

Council of Science Editors:

Denieul Y. Conception préliminaire de surfaces de contrôle et lois de commande pour configurations d’avions non conventionnelles : Preliminary Design of Control Surfaces and Laws for Unconventional Aircraft Configurations. [Doctoral Dissertation]. Toulouse, ISAE; 2016. Available from: http://www.theses.fr/2016ESAE0033

18. Saucez, Manuel. Résolution des qualités de vol de l'aile volante Airbus : Handling qualities resolution of the Airbus flying wing.

Degree: Docteur es, Mathématiques appliquées et Systèmes Embarqués, 2013, Toulouse, ISAE

L'objectif de cette étude est de résoudre les qualités de vol d'une aile volante long courrier, au stade de la conception avion. Le concept d'aile… (more)

Subjects/Keywords: Aile volante; Mécanique du vol; Conception avion; Optimisation; Handling qualities; Blended wing body; Control law; Conceptual design; Double split flaps; Thrust vectoring; Optimization; 621.39

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APA (6th Edition):

Saucez, M. (2013). Résolution des qualités de vol de l'aile volante Airbus : Handling qualities resolution of the Airbus flying wing. (Doctoral Dissertation). Toulouse, ISAE. Retrieved from http://www.theses.fr/2013ESAE0026

Chicago Manual of Style (16th Edition):

Saucez, Manuel. “Résolution des qualités de vol de l'aile volante Airbus : Handling qualities resolution of the Airbus flying wing.” 2013. Doctoral Dissertation, Toulouse, ISAE. Accessed January 24, 2021. http://www.theses.fr/2013ESAE0026.

MLA Handbook (7th Edition):

Saucez, Manuel. “Résolution des qualités de vol de l'aile volante Airbus : Handling qualities resolution of the Airbus flying wing.” 2013. Web. 24 Jan 2021.

Vancouver:

Saucez M. Résolution des qualités de vol de l'aile volante Airbus : Handling qualities resolution of the Airbus flying wing. [Internet] [Doctoral dissertation]. Toulouse, ISAE; 2013. [cited 2021 Jan 24]. Available from: http://www.theses.fr/2013ESAE0026.

Council of Science Editors:

Saucez M. Résolution des qualités de vol de l'aile volante Airbus : Handling qualities resolution of the Airbus flying wing. [Doctoral Dissertation]. Toulouse, ISAE; 2013. Available from: http://www.theses.fr/2013ESAE0026


Delft University of Technology

19. Scholten, Pepijn (author). A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion.

Degree: 2019, Delft University of Technology

Subjects/Keywords: Variable; Stability; In-Flight; Simulation; Handling; Qualities; Incremental; Non-linear; Dynamic; Inversion

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APA (6th Edition):

Scholten, P. (. (2019). A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:fbdfb1fe-b5a9-46b4-841c-27e4268a2925

Chicago Manual of Style (16th Edition):

Scholten, Pepijn (author). “A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion.” 2019. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:fbdfb1fe-b5a9-46b4-841c-27e4268a2925.

MLA Handbook (7th Edition):

Scholten, Pepijn (author). “A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion.” 2019. Web. 24 Jan 2021.

Vancouver:

Scholten P(. A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:fbdfb1fe-b5a9-46b4-841c-27e4268a2925.

Council of Science Editors:

Scholten P(. A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:fbdfb1fe-b5a9-46b4-841c-27e4268a2925


University of Maryland

20. Brown, Daniel Richard. EFFECTS OF CONTRAST AND SPATIAL FREQUENCY ON IDEALIZED COMPENSATORY TASKS.

Degree: Aerospace Engineering, 2014, University of Maryland

 The present analysis describes a series of experiments to quantify the effects of loss of contrast on highly-idealized, compensatory piloting tasks. The effects of spatial… (more)

Subjects/Keywords: Aerospace engineering; ADS-33; Degraded Visual Enviornments (DVE); Modulation Transfer Function (MTF); Rotorcraft Brownout; Rotorcraft Handling Qualities (HQ); Usable Cue Environment (UCE)

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APA (6th Edition):

Brown, D. R. (2014). EFFECTS OF CONTRAST AND SPATIAL FREQUENCY ON IDEALIZED COMPENSATORY TASKS. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/15446

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Brown, Daniel Richard. “EFFECTS OF CONTRAST AND SPATIAL FREQUENCY ON IDEALIZED COMPENSATORY TASKS.” 2014. Thesis, University of Maryland. Accessed January 24, 2021. http://hdl.handle.net/1903/15446.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Brown, Daniel Richard. “EFFECTS OF CONTRAST AND SPATIAL FREQUENCY ON IDEALIZED COMPENSATORY TASKS.” 2014. Web. 24 Jan 2021.

Vancouver:

Brown DR. EFFECTS OF CONTRAST AND SPATIAL FREQUENCY ON IDEALIZED COMPENSATORY TASKS. [Internet] [Thesis]. University of Maryland; 2014. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1903/15446.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Brown DR. EFFECTS OF CONTRAST AND SPATIAL FREQUENCY ON IDEALIZED COMPENSATORY TASKS. [Thesis]. University of Maryland; 2014. Available from: http://hdl.handle.net/1903/15446

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Pretoria

21. [No author]. Longitudinal handling characteristics of a tailless gull-wing aircraft .

Degree: 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

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APA (6th Edition):

author], [. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft . (Masters Thesis). University of Pretoria. Retrieved from http://upetd.up.ac.za/thesis/available/etd-09182008-132941/

Chicago Manual of Style (16th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Masters Thesis, University of Pretoria. Accessed January 24, 2021. http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

MLA Handbook (7th Edition):

author], [No. “Longitudinal handling characteristics of a tailless gull-wing aircraft .” 2008. Web. 24 Jan 2021.

Vancouver:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 24]. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/.

Council of Science Editors:

author] [. Longitudinal handling characteristics of a tailless gull-wing aircraft . [Masters Thesis]. University of Pretoria; 2008. Available from: http://upetd.up.ac.za/thesis/available/etd-09182008-132941/


University of Pretoria

22. Agenbag, Daniel Sarel. Longitudinal handling characteristics of a tailless gull-wing aircraft.

Degree: Mechanical and Aeronautical Engineering, 2008, University of Pretoria

 A handling quality investigation was performed on the swept gull-wing configuration. The swept gull-wing configuration is tailless and has a wing with a transition in… (more)

Subjects/Keywords: Flight simulation; Tumbling; Thumbprint criterion; Neal-smith analysis; C-star criterion; Shomber-gertsen analysis; Pilot induced oscillation; Oswald efficiency; Pilot mathematical model; Variable sweep wing; Exulans; Variable static margin; Swept gull-wing configuration; O-point; E-point; Handling qualities; Gust handling qualities; Tailless aircraft; Pecking; Monnich and dalldorff criterion; UCTD

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APA (6th Edition):

Agenbag, D. (2008). Longitudinal handling characteristics of a tailless gull-wing aircraft. (Masters Thesis). University of Pretoria. Retrieved from http://hdl.handle.net/2263/28011

Chicago Manual of Style (16th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Masters Thesis, University of Pretoria. Accessed January 24, 2021. http://hdl.handle.net/2263/28011.

MLA Handbook (7th Edition):

Agenbag, Daniel. “Longitudinal handling characteristics of a tailless gull-wing aircraft.” 2008. Web. 24 Jan 2021.

Vancouver:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Internet] [Masters thesis]. University of Pretoria; 2008. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2263/28011.

Council of Science Editors:

Agenbag D. Longitudinal handling characteristics of a tailless gull-wing aircraft. [Masters Thesis]. University of Pretoria; 2008. Available from: http://hdl.handle.net/2263/28011


Delft University of Technology

23. Yilmaz, D. Identification of manual control behaviour to assess rotorcraft handling qualities.

Degree: 2018, Delft University of Technology

 Flight safety has been a fundamental aspect of aircraft, and the future demand for wider usage of aerial operations leads to more focus on the… (more)

Subjects/Keywords: Rotorcraft; Handling Qualities; Adverse Rotorcraft Pilot Couplings; Manual Control Behaviour Identification; Pilot Modeling; Pilot Induced Oscillations

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APA (6th Edition):

Yilmaz, D. (2018). Identification of manual control behaviour to assess rotorcraft handling qualities. (Doctoral Dissertation). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; 00fadafa-0e24-4176-b533-d4b908c91a73 ; 10.4233/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:isbn:978-94-6186-966-1 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73

Chicago Manual of Style (16th Edition):

Yilmaz, D. “Identification of manual control behaviour to assess rotorcraft handling qualities.” 2018. Doctoral Dissertation, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; 00fadafa-0e24-4176-b533-d4b908c91a73 ; 10.4233/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:isbn:978-94-6186-966-1 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73.

MLA Handbook (7th Edition):

Yilmaz, D. “Identification of manual control behaviour to assess rotorcraft handling qualities.” 2018. Web. 24 Jan 2021.

Vancouver:

Yilmaz D. Identification of manual control behaviour to assess rotorcraft handling qualities. [Internet] [Doctoral dissertation]. Delft University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; 00fadafa-0e24-4176-b533-d4b908c91a73 ; 10.4233/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:isbn:978-94-6186-966-1 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73.

Council of Science Editors:

Yilmaz D. Identification of manual control behaviour to assess rotorcraft handling qualities. [Doctoral Dissertation]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; 00fadafa-0e24-4176-b533-d4b908c91a73 ; 10.4233/uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; urn:isbn:978-94-6186-966-1 ; urn:NBN:nl:ui:24-uuid:00fadafa-0e24-4176-b533-d4b908c91a73 ; http://resolver.tudelft.nl/uuid:00fadafa-0e24-4176-b533-d4b908c91a73


Georgia Tech

24. Potter, James Jackson. Input-shaped manual control of helicopters with suspended loads.

Degree: PhD, Mechanical Engineering, 2013, Georgia Tech

 A helicopter can be used to transport a load hanging from a suspension cable. This technique is frequently used in construction, firefighting, and disaster relief… (more)

Subjects/Keywords: Helicopter; Input shaping; Command filter; Sling load; Flexible system; Manual control; Human-in-the-loop control; Operator study; Handling qualities; Experimental platform; Dynamic modeling; Helicopters; Flight control; Cranes, derricks, etc. Dynamics; Feedback control systems; Damping (Mechanics)

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APA (6th Edition):

Potter, J. J. (2013). Input-shaped manual control of helicopters with suspended loads. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50342

Chicago Manual of Style (16th Edition):

Potter, James Jackson. “Input-shaped manual control of helicopters with suspended loads.” 2013. Doctoral Dissertation, Georgia Tech. Accessed January 24, 2021. http://hdl.handle.net/1853/50342.

MLA Handbook (7th Edition):

Potter, James Jackson. “Input-shaped manual control of helicopters with suspended loads.” 2013. Web. 24 Jan 2021.

Vancouver:

Potter JJ. Input-shaped manual control of helicopters with suspended loads. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1853/50342.

Council of Science Editors:

Potter JJ. Input-shaped manual control of helicopters with suspended loads. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50342


Brigham Young University

25. Foster, Tyler Michael. Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES.

Degree: MS, 2004, Brigham Young University

  General aircraft dynamic stability theory was used to predict the natural frequencies, damping ratios and time constants of the dynamic modes for three specific… (more)

Subjects/Keywords: Unmanned-Aerial-Vehicles; UAVs; UAV; Dynamic Stability; Static Stability; Handling Qualities; Flying Qualities; USAF DatCom; MIL-F-8785C; Dynamic Scaling; short period; phugoid; dutch-roll; spiral; roll; Mechanical Engineering

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APA (6th Edition):

Foster, T. M. (2004). Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1218&context=etd

Chicago Manual of Style (16th Edition):

Foster, Tyler Michael. “Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES.” 2004. Masters Thesis, Brigham Young University. Accessed January 24, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1218&context=etd.

MLA Handbook (7th Edition):

Foster, Tyler Michael. “Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES.” 2004. Web. 24 Jan 2021.

Vancouver:

Foster TM. Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES. [Internet] [Masters thesis]. Brigham Young University; 2004. [cited 2021 Jan 24]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1218&context=etd.

Council of Science Editors:

Foster TM. Dynamic Stability and Handling Qualities of Small Unmanned-Aerial-Vehicles UNMANNED-AERIAL-VEHICLES. [Masters Thesis]. Brigham Young University; 2004. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1218&context=etd

26. Tritschler, John. Contributions to the Characterization and Mitigation of Rotorcraft Brownout.

Degree: Aerospace Engineering, 2012, University of Maryland

 Rotorcraft brownout, the condition in which the flow field of a rotorcraft mobilizes sediment from the ground to generate a cloud that obscures the pilot's… (more)

Subjects/Keywords: Aerospace engineering; Degraded Visual Environments (DVE); Handling Qualities (HQ); Modulation Transfer Function (MTF); Rotorcraft brownout; Trajectory optimization

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Tritschler, J. (2012). Contributions to the Characterization and Mitigation of Rotorcraft Brownout. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/13061

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Tritschler, John. “Contributions to the Characterization and Mitigation of Rotorcraft Brownout.” 2012. Thesis, University of Maryland. Accessed January 24, 2021. http://hdl.handle.net/1903/13061.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Tritschler, John. “Contributions to the Characterization and Mitigation of Rotorcraft Brownout.” 2012. Web. 24 Jan 2021.

Vancouver:

Tritschler J. Contributions to the Characterization and Mitigation of Rotorcraft Brownout. [Internet] [Thesis]. University of Maryland; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1903/13061.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Tritschler J. Contributions to the Characterization and Mitigation of Rotorcraft Brownout. [Thesis]. University of Maryland; 2012. Available from: http://hdl.handle.net/1903/13061

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

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