Advanced search options

Advanced Search Options 🞨

Browse by author name (“Author name starts with…”).

Find ETDs with:

in
/  
in
/  
in
/  
in

Written in Published in Earliest date Latest date

Sorted by

Results per page:

Sorted by: relevance · author · university · dateNew search

You searched for subject:(Partial Integrated Guidance AND Control). Showing records 1 – 30 of 275 total matches.

[1] [2] [3] [4] [5] [6] [7] [8] [9] [10]

Search Limiters

Last 2 Years | English Only

Degrees

Levels

Country

▼ Search Limiters


Indian Institute of Science

1. Chawla, Charu. Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance.

Degree: 2010, Indian Institute of Science

 UAVs employed for low altitude jobs are more liable to collide with the urban structures on their way to the goal point. In this thesis,… (more)

Subjects/Keywords: Aircraft - Guidance & Control; Aircraft - Automatic Control; Obstacle Avoidance (Aeronautical Engineering); Partial Integrated Guidance and Control (PIGC); Aiming Point Guidance; Aeronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chawla, C. (2010). Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1659

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):

Chawla, Charu. “Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance.” 2010. Thesis, Indian Institute of Science. Accessed December 11, 2019. http://hdl.handle.net/2005/1659.

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

MLA Handbook (7th Edition):

Chawla, Charu. “Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance.” 2010. Web. 11 Dec 2019.

Vancouver:

Chawla C. Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance. [Internet] [Thesis]. Indian Institute of Science; 2010. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/2005/1659.

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

Council of Science Editors:

Chawla C. Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance. [Thesis]. Indian Institute of Science; 2010. Available from: http://hdl.handle.net/2005/1659

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


Indian Institute of Science

2. Chawla, Charu. Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance.

Degree: 2010, Indian Institute of Science

 UAVs employed for low altitude jobs are more liable to collide with the urban structures on their way to the goal point. In this thesis,… (more)

Subjects/Keywords: Aircraft - Guidance & Control; Aircraft - Automatic Control; Obstacle Avoidance (Aeronautical Engineering); Partial Integrated Guidance and Control (PIGC); Aiming Point Guidance; Aeronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Chawla, C. (2010). Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/1659 ; http://etd.ncsi.iisc.ernet.in/abstracts/2150/G24661-Abs.pdf

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):

Chawla, Charu. “Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance.” 2010. Thesis, Indian Institute of Science. Accessed December 11, 2019. http://etd.iisc.ernet.in/handle/2005/1659 ; http://etd.ncsi.iisc.ernet.in/abstracts/2150/G24661-Abs.pdf.

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

MLA Handbook (7th Edition):

Chawla, Charu. “Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance.” 2010. Web. 11 Dec 2019.

Vancouver:

Chawla C. Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance. [Internet] [Thesis]. Indian Institute of Science; 2010. [cited 2019 Dec 11]. Available from: http://etd.iisc.ernet.in/handle/2005/1659 ; http://etd.ncsi.iisc.ernet.in/abstracts/2150/G24661-Abs.pdf.

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

Council of Science Editors:

Chawla C. Robust Partial Integrated Guidance And Control Of UAVs For Reactive Obstacle Avoidance. [Thesis]. Indian Institute of Science; 2010. Available from: http://etd.iisc.ernet.in/handle/2005/1659 ; http://etd.ncsi.iisc.ernet.in/abstracts/2150/G24661-Abs.pdf

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


Indian Institute of Science

3. Das, Priya G. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.

Degree: 2009, Indian Institute of Science

 To address the concern of classical guidance and control designs (where guidance and control loops are designed separately in an “outer loop – inner loop”… (more)

Subjects/Keywords: Aerospace Vehicles - Guidance and Control; Interceptors (Aerospace Engineering); Guidance Systems (Flight); Flight Control; Endo-Atmospheric Interceptors; Partial Integrated Guidance and Control; Integrated Guidance and Control (IGC); Impact Angle Constraint; Astronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Das, P. G. (2009). Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1099

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):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2009. Thesis, Indian Institute of Science. Accessed December 11, 2019. http://hdl.handle.net/2005/1099.

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

MLA Handbook (7th Edition):

Das, Priya G. “Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors.” 2009. Web. 11 Dec 2019.

Vancouver:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/2005/1099.

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

Council of Science Editors:

Das PG. Time Scale Separated Nonlinear Partial Integrated Guidance And Control Of Endo-Atmospheric Interceptors. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1099

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


Purdue University

4. Kane, Anthony Mark. Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S).

Degree: MS, Aeronautics and Astronautics, 2014, Purdue University

  An integrated software architecture for development of unmanned research vehicles is developed. It has been created under the premise that all unmanned vehicles require… (more)

Subjects/Keywords: Applied sciences; Control; Guidance; Integrated flight software; Navigation; Aerospace Engineering; Computer Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kane, A. M. (2014). Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S). (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/338

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):

Kane, Anthony Mark. “Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S).” 2014. Thesis, Purdue University. Accessed December 11, 2019. http://docs.lib.purdue.edu/open_access_theses/338.

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

MLA Handbook (7th Edition):

Kane, Anthony Mark. “Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S).” 2014. Web. 11 Dec 2019.

Vancouver:

Kane AM. Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S). [Internet] [Thesis]. Purdue University; 2014. [cited 2019 Dec 11]. Available from: http://docs.lib.purdue.edu/open_access_theses/338.

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

Council of Science Editors:

Kane AM. Joint Architecture For Reusable Vehicle-Integrated Software (J.A.R.V.I.S). [Thesis]. Purdue University; 2014. Available from: http://docs.lib.purdue.edu/open_access_theses/338

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


Univerzitet u Beogradu

5. Pavić, Miloš V. 1972-. Нови алгоритми вођења ракете земља-ваздух средњег домета.

Degree: Mašinski fakultet, 2016, Univerzitet u Beogradu

Машинство - Војно машинство - системи наоружања / Mechanical engineering - Military engineering - weapon systems

У раду су дати нови закони вођења применљиви на… (more)

Subjects/Keywords: guidance; control; optimization; missile

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Pavić, M. V. 1. (2016). Нови алгоритми вођења ракете земља-ваздух средњег домета. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:11892/bdef:Content/get

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):

Pavić, Miloš V 1972-. “Нови алгоритми вођења ракете земља-ваздух средњег домета.” 2016. Thesis, Univerzitet u Beogradu. Accessed December 11, 2019. https://fedorabg.bg.ac.rs/fedora/get/o:11892/bdef:Content/get.

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

MLA Handbook (7th Edition):

Pavić, Miloš V 1972-. “Нови алгоритми вођења ракете земља-ваздух средњег домета.” 2016. Web. 11 Dec 2019.

Vancouver:

Pavić MV1. Нови алгоритми вођења ракете земља-ваздух средњег домета. [Internet] [Thesis]. Univerzitet u Beogradu; 2016. [cited 2019 Dec 11]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:11892/bdef:Content/get.

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

Council of Science Editors:

Pavić MV1. Нови алгоритми вођења ракете земља-ваздух средњег домета. [Thesis]. Univerzitet u Beogradu; 2016. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:11892/bdef:Content/get

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


Georgia Tech

6. Sattigeri, Ramachandra Jayant. Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight.

Degree: PhD, Aerospace Engineering, 2007, Georgia Tech

 The role of vision as an additional sensing mechanism has received a lot of attention in recent years in the context of autonomous flight applications.… (more)

Subjects/Keywords: Neural networks; Target tracking; Adaptive estimation; Adaptive Kalman filters; Integrated guidance and control; Adaptive guidance and control; Adaptive control; Unmanned aerial vehicles; Multiple-vehicle formation; Guidance systems (Flight); Robot vision; Adaptive control systems; Drone aircraft; Flight control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Sattigeri, R. J. (2007). Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/16272

Chicago Manual of Style (16th Edition):

Sattigeri, Ramachandra Jayant. “Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight.” 2007. Doctoral Dissertation, Georgia Tech. Accessed December 11, 2019. http://hdl.handle.net/1853/16272.

MLA Handbook (7th Edition):

Sattigeri, Ramachandra Jayant. “Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight.” 2007. Web. 11 Dec 2019.

Vancouver:

Sattigeri RJ. Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight. [Internet] [Doctoral dissertation]. Georgia Tech; 2007. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1853/16272.

Council of Science Editors:

Sattigeri RJ. Adaptive Estimation and Control with Application to Vision-based Autonomous Formation Flight. [Doctoral Dissertation]. Georgia Tech; 2007. Available from: http://hdl.handle.net/1853/16272


Indian Institute of Science

7. Kumar, Shashi Ranjan. Sliding Mode Control Based Guidance Strategies with Terminal Constraints.

Degree: 2015, Indian Institute of Science

 In the guidance literature, minimizing miss distance along with optimizing the energy usage had been an objective for several decades. In current day applications, additional… (more)

Subjects/Keywords: Sliding Mode Control; Guidance and Control Theory; Sliding Mode Guidance Laws; Impact Angle Guidance; Impact Time Guidance; Guidance Laws; Sliding Mode Guidance; Salvo Attack Guidance; Nonlinear Engagement Dynamics; Missile Guidance; Flight Control; Finite Time Convergence; Sliding-Mode Guidance; Impact Time Guidance; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kumar, S. R. (2015). Sliding Mode Control Based Guidance Strategies with Terminal Constraints. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf

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):

Kumar, Shashi Ranjan. “Sliding Mode Control Based Guidance Strategies with Terminal Constraints.” 2015. Thesis, Indian Institute of Science. Accessed December 11, 2019. http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf.

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

MLA Handbook (7th Edition):

Kumar, Shashi Ranjan. “Sliding Mode Control Based Guidance Strategies with Terminal Constraints.” 2015. Web. 11 Dec 2019.

Vancouver:

Kumar SR. Sliding Mode Control Based Guidance Strategies with Terminal Constraints. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Dec 11]. Available from: http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf.

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

Council of Science Editors:

Kumar SR. Sliding Mode Control Based Guidance Strategies with Terminal Constraints. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3876 ; http://etd.iisc.ernet.in/abstracts/4748/G26895-Abs.pdf

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


Univerzitet u Beogradu

8. Todić, Ivana S., 1983-. Optimalno vođenje u uslovima velikih poremećaja i ograničenih performanski leta rakete.

Degree: Mašinski fakultet, 2016, Univerzitet u Beogradu

Mašinstvo - Vojno mašinstvo - Sistemi naoružanja / mechanical engineering - Military engineering

U doktorskoj tezi je urađena analiza kretanja, vođenja i upravljanja za koncept rakete sa ležajem odvojenim sekcijama...

Advisors/Committee Members: Jaramaz, Slobodan, 1952-.

Subjects/Keywords: guidance laws; adaptive control; autopilot; inertial navigation

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Todić, Ivana S., 1. (2016). Optimalno vođenje u uslovima velikih poremećaja i ograničenih performanski leta rakete. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:12811/bdef:Content/get

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):

Todić, Ivana S., 1983-. “Optimalno vođenje u uslovima velikih poremećaja i ograničenih performanski leta rakete.” 2016. Thesis, Univerzitet u Beogradu. Accessed December 11, 2019. https://fedorabg.bg.ac.rs/fedora/get/o:12811/bdef:Content/get.

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

MLA Handbook (7th Edition):

Todić, Ivana S., 1983-. “Optimalno vođenje u uslovima velikih poremećaja i ograničenih performanski leta rakete.” 2016. Web. 11 Dec 2019.

Vancouver:

Todić, Ivana S. 1. Optimalno vođenje u uslovima velikih poremećaja i ograničenih performanski leta rakete. [Internet] [Thesis]. Univerzitet u Beogradu; 2016. [cited 2019 Dec 11]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:12811/bdef:Content/get.

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

Council of Science Editors:

Todić, Ivana S. 1. Optimalno vođenje u uslovima velikih poremećaja i ograničenih performanski leta rakete. [Thesis]. Univerzitet u Beogradu; 2016. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:12811/bdef:Content/get

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

9. Steindorf, Lukas. Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission.

Degree: Electrical and Space Engineering, 2017, Luleå University of Technology

  This thesis proposes a continuous low-thrust guidance and control strategy for satellite formation-flying. Stabilizing feedback based on mean relative orbit elements and Lyapunov theory… (more)

Subjects/Keywords: satellite; formation; control; guidance; continuous; low-thrust

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Steindorf, L. (2017). Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61599

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):

Steindorf, Lukas. “Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission.” 2017. Thesis, Luleå University of Technology. Accessed December 11, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61599.

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

MLA Handbook (7th Edition):

Steindorf, Lukas. “Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission.” 2017. Web. 11 Dec 2019.

Vancouver:

Steindorf L. Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission. [Internet] [Thesis]. Luleå University of Technology; 2017. [cited 2019 Dec 11]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61599.

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

Council of Science Editors:

Steindorf L. Constrained Low-Thrust Satellite Formation-Flying Using Relative Orbit Elements : Autonomous Guidance and Control for the NetSat Satellite Formation-Flying Mission. [Thesis]. Luleå University of Technology; 2017. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-61599

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


University of Johannesburg

10. Petty, Ruth Ann. The issue of control in the therapeutic relationship.

Degree: 2014, University of Johannesburg

M.A. (Clinical Psychology)

It was deemed important to undertake a study on control, because divergent approaches toward the issue of control emerged, which have important… (more)

Subjects/Keywords: Clinical psychology; Psychotherapy - Vocational guidance; Control (Psychology)

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Petty, R. A. (2014). The issue of control in the therapeutic relationship. (Thesis). University of Johannesburg. Retrieved from http://hdl.handle.net/10210/10093

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):

Petty, Ruth Ann. “The issue of control in the therapeutic relationship.” 2014. Thesis, University of Johannesburg. Accessed December 11, 2019. http://hdl.handle.net/10210/10093.

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

MLA Handbook (7th Edition):

Petty, Ruth Ann. “The issue of control in the therapeutic relationship.” 2014. Web. 11 Dec 2019.

Vancouver:

Petty RA. The issue of control in the therapeutic relationship. [Internet] [Thesis]. University of Johannesburg; 2014. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/10210/10093.

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

Council of Science Editors:

Petty RA. The issue of control in the therapeutic relationship. [Thesis]. University of Johannesburg; 2014. Available from: http://hdl.handle.net/10210/10093

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


Cal Poly

11. Iuliano, Jay R. A Solution to the Circular Restricted N Body Problem in Planetary Systems.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  This thesis is a brief look at a new solution to a problem that has been approached in many different ways in the past… (more)

Subjects/Keywords: Astrodynamics; Navigation, Guidance, Control and Dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Iuliano, J. R. (2016). A Solution to the Circular Restricted N Body Problem in Planetary Systems. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80

Chicago Manual of Style (16th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Masters Thesis, Cal Poly. Accessed December 11, 2019. https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

MLA Handbook (7th Edition):

Iuliano, Jay R. “A Solution to the Circular Restricted N Body Problem in Planetary Systems.” 2016. Web. 11 Dec 2019.

Vancouver:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Dec 11]. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80.

Council of Science Editors:

Iuliano JR. A Solution to the Circular Restricted N Body Problem in Planetary Systems. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1612 ; 10.15368/theses.2016.80


University of Illinois – Urbana-Champaign

12. Foust, Rebecca C. Optimal guidance and control of heterogeneous swarms for in-orbit self-assembly of large space structures: Algorithms and experiments.

Degree: PhD, Aerospace Engineering, 2019, University of Illinois – Urbana-Champaign

 Satellite design has been harshly constrained by surviving entry into space though the majority of the satellite's lifetime exists in much calmer conditions. Significant study… (more)

Subjects/Keywords: optimal swarm guidance and control; space robotics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Foust, R. C. (2019). Optimal guidance and control of heterogeneous swarms for in-orbit self-assembly of large space structures: Algorithms and experiments. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/105684

Chicago Manual of Style (16th Edition):

Foust, Rebecca C. “Optimal guidance and control of heterogeneous swarms for in-orbit self-assembly of large space structures: Algorithms and experiments.” 2019. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed December 11, 2019. http://hdl.handle.net/2142/105684.

MLA Handbook (7th Edition):

Foust, Rebecca C. “Optimal guidance and control of heterogeneous swarms for in-orbit self-assembly of large space structures: Algorithms and experiments.” 2019. Web. 11 Dec 2019.

Vancouver:

Foust RC. Optimal guidance and control of heterogeneous swarms for in-orbit self-assembly of large space structures: Algorithms and experiments. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2019. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/2142/105684.

Council of Science Editors:

Foust RC. Optimal guidance and control of heterogeneous swarms for in-orbit self-assembly of large space structures: Algorithms and experiments. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2019. Available from: http://hdl.handle.net/2142/105684


Indian Institute of Science

13. Abdul Saleem, P K. Guidance Laws for Engagement Time Control.

Degree: 2016, Indian Institute of Science

 Autonomous aerial vehicles like missiles and unmanned aerial vehicles (UAVs) have attracted various military and civilian applications. The primary guidance objective of any autonomous vehicle… (more)

Subjects/Keywords: Unmanned Aerial Vehicles; Missile Impact Time Control; Guidance Laws; Missile Guidance; Impact Time Control Guidance Law; Unmanned Aerial Vehcile Arrival Time Control; Lyapunov Guidance Law; Unmanned Aerial Vehicle Guidance; Nonlinear Guidance Laws; Autonomous Aerial Vehicles; Missiles; Salvo Attack; Impact Time Control; UAVs; Aerospace Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Abdul Saleem, P. K. (2016). Guidance Laws for Engagement Time Control. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2926

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):

Abdul Saleem, P K. “Guidance Laws for Engagement Time Control.” 2016. Thesis, Indian Institute of Science. Accessed December 11, 2019. http://hdl.handle.net/2005/2926.

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

MLA Handbook (7th Edition):

Abdul Saleem, P K. “Guidance Laws for Engagement Time Control.” 2016. Web. 11 Dec 2019.

Vancouver:

Abdul Saleem PK. Guidance Laws for Engagement Time Control. [Internet] [Thesis]. Indian Institute of Science; 2016. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/2005/2926.

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

Council of Science Editors:

Abdul Saleem PK. Guidance Laws for Engagement Time Control. [Thesis]. Indian Institute of Science; 2016. Available from: http://hdl.handle.net/2005/2926

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


Cal Poly

14. KATO, TOMOYUKI. Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification.

Degree: MS, Aerospace Engineering, 2014, Cal Poly

  The Cal Poly Spacecraft Dynamics Simulator, also known as the Pyramidal Reaction Wheel Platform (PRWP), is an air-bearing four reaction wheel spacecraft simulator designed… (more)

Subjects/Keywords: Spacecraft; Simulator; Adaptive; Control; Robust; Navigation, Guidance, Control and Dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

KATO, T. (2014). Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48

Chicago Manual of Style (16th Edition):

KATO, TOMOYUKI. “Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification.” 2014. Masters Thesis, Cal Poly. Accessed December 11, 2019. https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48.

MLA Handbook (7th Edition):

KATO, TOMOYUKI. “Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification.” 2014. Web. 11 Dec 2019.

Vancouver:

KATO T. Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification. [Internet] [Masters thesis]. Cal Poly; 2014. [cited 2019 Dec 11]. Available from: https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48.

Council of Science Editors:

KATO T. Modification of the Cal Poly Spacecraft Simulator System for Robust Control Law Verification. [Masters Thesis]. Cal Poly; 2014. Available from: https://digitalcommons.calpoly.edu/theses/1201 ; 10.15368/theses.2014.48


Indian Institute of Science

15. Raghunathan, T. Differential Evolution Based Interceptor Guidance Law.

Degree: 2011, Indian Institute of Science

 Kinematics based guidance laws like the proportional navigation (PN) and many other linear optimal guidance laws perform well in near-collision course conditions. These have been… (more)

Subjects/Keywords: Aircraft - Guidance & Control; Airplanes - Navigation; 2-D Kinematic Model; 3-D Guidance Law; Guidance Law; Aeronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Raghunathan, T. (2011). Differential Evolution Based Interceptor Guidance Law. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2014

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):

Raghunathan, T. “Differential Evolution Based Interceptor Guidance Law.” 2011. Thesis, Indian Institute of Science. Accessed December 11, 2019. http://hdl.handle.net/2005/2014.

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

MLA Handbook (7th Edition):

Raghunathan, T. “Differential Evolution Based Interceptor Guidance Law.” 2011. Web. 11 Dec 2019.

Vancouver:

Raghunathan T. Differential Evolution Based Interceptor Guidance Law. [Internet] [Thesis]. Indian Institute of Science; 2011. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/2005/2014.

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

Council of Science Editors:

Raghunathan T. Differential Evolution Based Interceptor Guidance Law. [Thesis]. Indian Institute of Science; 2011. Available from: http://hdl.handle.net/2005/2014

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


Indian Institute of Science

16. Raghunathan, T. Differential Evolution Based Interceptor Guidance Law.

Degree: 2011, Indian Institute of Science

 Kinematics based guidance laws like the proportional navigation (PN) and many other linear optimal guidance laws perform well in near-collision course conditions. These have been… (more)

Subjects/Keywords: Aircraft - Guidance & Control; Airplanes - Navigation; 2-D Kinematic Model; 3-D Guidance Law; Guidance Law; Aeronautics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Raghunathan, T. (2011). Differential Evolution Based Interceptor Guidance Law. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2014 ; http://etd.ncsi.iisc.ernet.in/abstracts/2608/G25096-Abs.pdf

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):

Raghunathan, T. “Differential Evolution Based Interceptor Guidance Law.” 2011. Thesis, Indian Institute of Science. Accessed December 11, 2019. http://etd.iisc.ernet.in/handle/2005/2014 ; http://etd.ncsi.iisc.ernet.in/abstracts/2608/G25096-Abs.pdf.

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

MLA Handbook (7th Edition):

Raghunathan, T. “Differential Evolution Based Interceptor Guidance Law.” 2011. Web. 11 Dec 2019.

Vancouver:

Raghunathan T. Differential Evolution Based Interceptor Guidance Law. [Internet] [Thesis]. Indian Institute of Science; 2011. [cited 2019 Dec 11]. Available from: http://etd.iisc.ernet.in/handle/2005/2014 ; http://etd.ncsi.iisc.ernet.in/abstracts/2608/G25096-Abs.pdf.

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

Council of Science Editors:

Raghunathan T. Differential Evolution Based Interceptor Guidance Law. [Thesis]. Indian Institute of Science; 2011. Available from: http://etd.iisc.ernet.in/handle/2005/2014 ; http://etd.ncsi.iisc.ernet.in/abstracts/2608/G25096-Abs.pdf

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


KTH

17. Sefastsson, Ulf. Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model.

Degree: Optimization and Systems Theory, 2016, KTH

Missile guidance and autopilot have been active fields of research since the second world war. There are lots of literature on the subjects, but… (more)

Subjects/Keywords: Missile Guidance; Proportional Navigation; Optimal Guidance; Differential Game Guidance; Model Predictive Control.; Missilstyrning; syftbäringsstyrning; optimal missilstyrning; spelteoretisk missilstyrning; modellprediktiv reglering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Sefastsson, U. (2016). Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897

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):

Sefastsson, Ulf. “Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model.” 2016. Thesis, KTH. Accessed December 11, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897.

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

MLA Handbook (7th Edition):

Sefastsson, Ulf. “Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model.” 2016. Web. 11 Dec 2019.

Vancouver:

Sefastsson U. Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model. [Internet] [Thesis]. KTH; 2016. [cited 2019 Dec 11]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897.

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

Council of Science Editors:

Sefastsson U. Evaluation of Missile Guidance and Autopilot through a 6 DOF Simulation Model. [Thesis]. KTH; 2016. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-188897

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

18. Tran, Thanh Trung. Nonlinear Flight Control Design Using Backstepping Methodology.

Degree: PhD, Aerospace Engineering, 2016, Old Dominion University

  The subject of nonlinear flight control design using backstepping control methodology is investigated in the dissertation research presented here. Control design methods based on… (more)

Subjects/Keywords: Backstepping control; Lyapunov-Based Design; Nonlinear flight control; Aerospace Engineering; Navigation, Guidance, Control and Dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Tran, T. T. (2016). Nonlinear Flight Control Design Using Backstepping Methodology. (Doctoral Dissertation). Old Dominion University. Retrieved from 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16

Chicago Manual of Style (16th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Doctoral Dissertation, Old Dominion University. Accessed December 11, 2019. 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

MLA Handbook (7th Edition):

Tran, Thanh Trung. “Nonlinear Flight Control Design Using Backstepping Methodology.” 2016. Web. 11 Dec 2019.

Vancouver:

Tran TT. Nonlinear Flight Control Design Using Backstepping Methodology. [Internet] [Doctoral dissertation]. Old Dominion University; 2016. [cited 2019 Dec 11]. Available from: 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16.

Council of Science Editors:

Tran TT. Nonlinear Flight Control Design Using Backstepping Methodology. [Doctoral Dissertation]. Old Dominion University; 2016. Available from: 9781369169768 ; https://digitalcommons.odu.edu/mae_etds/16


University of Illinois – Urbana-Champaign

19. Li, Zhiyuan. Guidance, control and estimation of autonomous vehicle systems.

Degree: PhD, 0133, 2014, University of Illinois – Urbana-Champaign

 This research focuses on designing practical guidance, control and estimation algorithms for autonomous vehicle systems. The objective is to provide robust control and estimation algorithms… (more)

Subjects/Keywords: autonomous system; unmanned system; distributed control; Adaptive Control; cooperative control; vision based guidance

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Li, Z. (2014). Guidance, control and estimation of autonomous vehicle systems. (Doctoral Dissertation). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/46871

Chicago Manual of Style (16th Edition):

Li, Zhiyuan. “Guidance, control and estimation of autonomous vehicle systems.” 2014. Doctoral Dissertation, University of Illinois – Urbana-Champaign. Accessed December 11, 2019. http://hdl.handle.net/2142/46871.

MLA Handbook (7th Edition):

Li, Zhiyuan. “Guidance, control and estimation of autonomous vehicle systems.” 2014. Web. 11 Dec 2019.

Vancouver:

Li Z. Guidance, control and estimation of autonomous vehicle systems. [Internet] [Doctoral dissertation]. University of Illinois – Urbana-Champaign; 2014. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/2142/46871.

Council of Science Editors:

Li Z. Guidance, control and estimation of autonomous vehicle systems. [Doctoral Dissertation]. University of Illinois – Urbana-Champaign; 2014. Available from: http://hdl.handle.net/2142/46871


Cal Poly

20. Villa, Andres Eduardo. Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.

Degree: MS, Aerospace Engineering, 2016, Cal Poly

  Due to mass and volume constraints on planetary missions, the development of control techniques that do not require fuel are of big interest. For… (more)

Subjects/Keywords: Mars; Formation Flying; Proximity Operations; Differential Drag; Lyapunov; Control Theory; Guidance; Navigation; Perturbations; Aerospace Engineering; Astrodynamics; Navigation, Guidance, Control and Dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Villa, A. E. (2016). Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48

Chicago Manual of Style (16th Edition):

Villa, Andres Eduardo. “Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.” 2016. Masters Thesis, Cal Poly. Accessed December 11, 2019. https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48.

MLA Handbook (7th Edition):

Villa, Andres Eduardo. “Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere.” 2016. Web. 11 Dec 2019.

Vancouver:

Villa AE. Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere. [Internet] [Masters thesis]. Cal Poly; 2016. [cited 2019 Dec 11]. Available from: https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48.

Council of Science Editors:

Villa AE. Autonomous Formation Flying and Proximity Operations Using Differential Drag on the Mars Atmosphere. [Masters Thesis]. Cal Poly; 2016. Available from: https://digitalcommons.calpoly.edu/theses/1571 ; 10.15368/theses.2016.48


Embry-Riddle Aeronautical University

21. Hervás, Jaime Rubio. Dynamics and Control of Higher-order Nonholonomic Systems.

Degree: PhD, Doctoral Studies, 2013, Embry-Riddle Aeronautical University

  A theoretical framework is established for the control of higher-order nonholonomic systems, defined as systems that satisfy higher-order nonintegrable constraints. A model for such… (more)

Subjects/Keywords: Aerospace Engineering; Navigation, Guidance, Control and Dynamics; Robotics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hervás, J. R. (2013). Dynamics and Control of Higher-order Nonholonomic Systems. (Doctoral Dissertation). Embry-Riddle Aeronautical University. Retrieved from http://commons.erau.edu/edt/154

Chicago Manual of Style (16th Edition):

Hervás, Jaime Rubio. “Dynamics and Control of Higher-order Nonholonomic Systems.” 2013. Doctoral Dissertation, Embry-Riddle Aeronautical University. Accessed December 11, 2019. http://commons.erau.edu/edt/154.

MLA Handbook (7th Edition):

Hervás, Jaime Rubio. “Dynamics and Control of Higher-order Nonholonomic Systems.” 2013. Web. 11 Dec 2019.

Vancouver:

Hervás JR. Dynamics and Control of Higher-order Nonholonomic Systems. [Internet] [Doctoral dissertation]. Embry-Riddle Aeronautical University; 2013. [cited 2019 Dec 11]. Available from: http://commons.erau.edu/edt/154.

Council of Science Editors:

Hervás JR. Dynamics and Control of Higher-order Nonholonomic Systems. [Doctoral Dissertation]. Embry-Riddle Aeronautical University; 2013. Available from: http://commons.erau.edu/edt/154


Georgia Tech

22. Scheuermann, Edward J. Autonomous control of parafoil and payload systems using upper surface canopy spoilers.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 With the advent of steerable, ram air parafoil canopies, aerial payload delivery has become a viable alternative for situations involving remote or undeveloped areas, hostile… (more)

Subjects/Keywords: Airdrop systems; Autonomous control; Dynamic modeling; Guidance; Parachutes; Parafoils; Aerodynamic spoilers

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Scheuermann, E. J. (2015). Autonomous control of parafoil and payload systems using upper surface canopy spoilers. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53874

Chicago Manual of Style (16th Edition):

Scheuermann, Edward J. “Autonomous control of parafoil and payload systems using upper surface canopy spoilers.” 2015. Doctoral Dissertation, Georgia Tech. Accessed December 11, 2019. http://hdl.handle.net/1853/53874.

MLA Handbook (7th Edition):

Scheuermann, Edward J. “Autonomous control of parafoil and payload systems using upper surface canopy spoilers.” 2015. Web. 11 Dec 2019.

Vancouver:

Scheuermann EJ. Autonomous control of parafoil and payload systems using upper surface canopy spoilers. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1853/53874.

Council of Science Editors:

Scheuermann EJ. Autonomous control of parafoil and payload systems using upper surface canopy spoilers. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53874


Lehigh University

23. Hau, Yu Hin. Guidance, Navigation and Control System of a Hopper Spacecraft Simulator.

Degree: MS, Mechanical Engineering, 2015, Lehigh University

 The space hopper simulator project drew its origin from a partnership with Penn State University to compete in the Google Lunar XPRIZE competition. Lehigh University… (more)

Subjects/Keywords: Control; Guidance; Hopper; Naviation; Quadcopter; Spacecraft; Engineering; Mechanical Engineering

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Hau, Y. H. (2015). Guidance, Navigation and Control System of a Hopper Spacecraft Simulator. (Thesis). Lehigh University. Retrieved from https://preserve.lehigh.edu/etd/2630

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):

Hau, Yu Hin. “Guidance, Navigation and Control System of a Hopper Spacecraft Simulator.” 2015. Thesis, Lehigh University. Accessed December 11, 2019. https://preserve.lehigh.edu/etd/2630.

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

MLA Handbook (7th Edition):

Hau, Yu Hin. “Guidance, Navigation and Control System of a Hopper Spacecraft Simulator.” 2015. Web. 11 Dec 2019.

Vancouver:

Hau YH. Guidance, Navigation and Control System of a Hopper Spacecraft Simulator. [Internet] [Thesis]. Lehigh University; 2015. [cited 2019 Dec 11]. Available from: https://preserve.lehigh.edu/etd/2630.

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

Council of Science Editors:

Hau YH. Guidance, Navigation and Control System of a Hopper Spacecraft Simulator. [Thesis]. Lehigh University; 2015. Available from: https://preserve.lehigh.edu/etd/2630

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


University of Victoria

24. Buchanan, M. Amos. Characterization and Control of a Saab Seaeye Thruster.

Degree: Department of Mechanical Engineering, 2015, University of Victoria

 The use of Remotely Operated Vehicles (ROVs) in exploring and building infrastructure in the ocean is expanding. ROVs are performing tasks underwater that would be… (more)

Subjects/Keywords: Thruster Control; Ocean; Remote Underwater Vehicle; ROV; Underwater Thruster; Guidance

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Buchanan, M. A. (2015). Characterization and Control of a Saab Seaeye Thruster. (Masters Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/6003

Chicago Manual of Style (16th Edition):

Buchanan, M Amos. “Characterization and Control of a Saab Seaeye Thruster.” 2015. Masters Thesis, University of Victoria. Accessed December 11, 2019. http://hdl.handle.net/1828/6003.

MLA Handbook (7th Edition):

Buchanan, M Amos. “Characterization and Control of a Saab Seaeye Thruster.” 2015. Web. 11 Dec 2019.

Vancouver:

Buchanan MA. Characterization and Control of a Saab Seaeye Thruster. [Internet] [Masters thesis]. University of Victoria; 2015. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/1828/6003.

Council of Science Editors:

Buchanan MA. Characterization and Control of a Saab Seaeye Thruster. [Masters Thesis]. University of Victoria; 2015. Available from: http://hdl.handle.net/1828/6003


Virginia Tech

25. Balasubramanian, Balasundar. A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints.

Degree: MS, Electrical and Computer Engineering, 2010, Virginia Tech

 We present a new trajectory generation algorithm for autonomous guidance and control of unmanned vehicles from a given starting point to a given target location.… (more)

Subjects/Keywords: path planning; guidance; trajectory generation; unmanned vehicles; receding horizon control

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Balasubramanian, B. (2010). A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/36430

Chicago Manual of Style (16th Edition):

Balasubramanian, Balasundar. “A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints.” 2010. Masters Thesis, Virginia Tech. Accessed December 11, 2019. http://hdl.handle.net/10919/36430.

MLA Handbook (7th Edition):

Balasubramanian, Balasundar. “A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints.” 2010. Web. 11 Dec 2019.

Vancouver:

Balasubramanian B. A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints. [Internet] [Masters thesis]. Virginia Tech; 2010. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/10919/36430.

Council of Science Editors:

Balasubramanian B. A new guidance trajectory generation algorithm for unmanned systems incorporating vehicle dynamics and constraints. [Masters Thesis]. Virginia Tech; 2010. Available from: http://hdl.handle.net/10919/36430


Curtin University of Technology

26. Zhou, Jingyang. Optimal guidance and control in space technology .

Degree: 2011, Curtin University of Technology

 In this thesis, we deal with several optimal guidance and control problems of the spacecrafts arising from the study of lunar exploration. The research is… (more)

Subjects/Keywords: optimal guidance; space-crafts; lunar exploration; control problems

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Zhou, J. (2011). Optimal guidance and control in space technology . (Thesis). Curtin University of Technology. Retrieved from http://hdl.handle.net/20.500.11937/1503

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):

Zhou, Jingyang. “Optimal guidance and control in space technology .” 2011. Thesis, Curtin University of Technology. Accessed December 11, 2019. http://hdl.handle.net/20.500.11937/1503.

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

MLA Handbook (7th Edition):

Zhou, Jingyang. “Optimal guidance and control in space technology .” 2011. Web. 11 Dec 2019.

Vancouver:

Zhou J. Optimal guidance and control in space technology . [Internet] [Thesis]. Curtin University of Technology; 2011. [cited 2019 Dec 11]. Available from: http://hdl.handle.net/20.500.11937/1503.

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

Council of Science Editors:

Zhou J. Optimal guidance and control in space technology . [Thesis]. Curtin University of Technology; 2011. Available from: http://hdl.handle.net/20.500.11937/1503

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


Luleå University of Technology

27. Luque, Santiago Peña. Optimal guidance for space applications.

Degree: 2009, Luleå University of Technology

The first part of this study was focused on describe the state-of-art in optimization techniques for general space operations, and especially in landing operations.… (more)

Subjects/Keywords: Technology; GNC; DIDO; optimal control; guidance; optimization; asteroid; landing; Teknik

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Luque, S. P. (2009). Optimal guidance for space applications. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-46801

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):

Luque, Santiago Peña. “Optimal guidance for space applications.” 2009. Thesis, Luleå University of Technology. Accessed December 11, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-46801.

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

MLA Handbook (7th Edition):

Luque, Santiago Peña. “Optimal guidance for space applications.” 2009. Web. 11 Dec 2019.

Vancouver:

Luque SP. Optimal guidance for space applications. [Internet] [Thesis]. Luleå University of Technology; 2009. [cited 2019 Dec 11]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-46801.

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

Council of Science Editors:

Luque SP. Optimal guidance for space applications. [Thesis]. Luleå University of Technology; 2009. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-46801

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


Delft University of Technology

28. De Nijs, S.Y. The Power of Haptic Guidance:.

Degree: 2011, Delft University of Technology

 Background: Haptic guidance is a continuous form of haptic feedback where the driver obtains information through small corrective forces on control inputs, such as the… (more)

Subjects/Keywords: Haptic Guidance; curve negotiation; control information; visual occlusion

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

De Nijs, S. Y. (2011). The Power of Haptic Guidance:. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:8b8e120e-5821-4b70-9114-c243a55c9f40

Chicago Manual of Style (16th Edition):

De Nijs, S Y. “The Power of Haptic Guidance:.” 2011. Masters Thesis, Delft University of Technology. Accessed December 11, 2019. http://resolver.tudelft.nl/uuid:8b8e120e-5821-4b70-9114-c243a55c9f40.

MLA Handbook (7th Edition):

De Nijs, S Y. “The Power of Haptic Guidance:.” 2011. Web. 11 Dec 2019.

Vancouver:

De Nijs SY. The Power of Haptic Guidance:. [Internet] [Masters thesis]. Delft University of Technology; 2011. [cited 2019 Dec 11]. Available from: http://resolver.tudelft.nl/uuid:8b8e120e-5821-4b70-9114-c243a55c9f40.

Council of Science Editors:

De Nijs SY. The Power of Haptic Guidance:. [Masters Thesis]. Delft University of Technology; 2011. Available from: http://resolver.tudelft.nl/uuid:8b8e120e-5821-4b70-9114-c243a55c9f40


University of Tennessee – Knoxville

29. Kamp, Michael Anthony. Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet.

Degree: MS, Aviation Systems, 2009, University of Tennessee – Knoxville

 A self-contained, portable, inertial and positional measurement system was developed and tested for an HGU-55 model fighter pilot helmet. The system, designated the Portable Helmet… (more)

Subjects/Keywords: Navigation; Guidance; Control and Dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Kamp, M. A. (2009). Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/535

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):

Kamp, Michael Anthony. “Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet.” 2009. Thesis, University of Tennessee – Knoxville. Accessed December 11, 2019. https://trace.tennessee.edu/utk_gradthes/535.

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

MLA Handbook (7th Edition):

Kamp, Michael Anthony. “Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet.” 2009. Web. 11 Dec 2019.

Vancouver:

Kamp MA. Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet. [Internet] [Thesis]. University of Tennessee – Knoxville; 2009. [cited 2019 Dec 11]. Available from: https://trace.tennessee.edu/utk_gradthes/535.

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

Council of Science Editors:

Kamp MA. Development and Testing of a Self-Contained, Portable Instrumentation System for a Fighter Pilot Helmet. [Thesis]. University of Tennessee – Knoxville; 2009. Available from: https://trace.tennessee.edu/utk_gradthes/535

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


University of Tennessee – Knoxville

30. Schrum, Brian T. F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings.

Degree: MS, Aviation Systems, 2007, University of Tennessee – Knoxville

  The purpose for writing this thesis is to prove the automatic carrier landing system (ACLS) a valuable Operational Risk Management (ORM) tool for recovering… (more)

Subjects/Keywords: Navigation; Guidance; Control and Dynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Schrum, B. T. (2007). F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/323

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):

Schrum, Brian T. “F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings.” 2007. Thesis, University of Tennessee – Knoxville. Accessed December 11, 2019. https://trace.tennessee.edu/utk_gradthes/323.

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

MLA Handbook (7th Edition):

Schrum, Brian T. “F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings.” 2007. Web. 11 Dec 2019.

Vancouver:

Schrum BT. F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings. [Internet] [Thesis]. University of Tennessee – Knoxville; 2007. [cited 2019 Dec 11]. Available from: https://trace.tennessee.edu/utk_gradthes/323.

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

Council of Science Editors:

Schrum BT. F/A-18A-D Hornet Current and Future Utilization of Mode I Automatic Carrier Landings. [Thesis]. University of Tennessee – Knoxville; 2007. Available from: https://trace.tennessee.edu/utk_gradthes/323

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

[1] [2] [3] [4] [5] [6] [7] [8] [9] [10]

.