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You searched for subject:(Impact Angle Guidance). Showing records 1 – 6 of 6 total matches.

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Indian Institute of Science

1. 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

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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 10, 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. 10 Dec 2019.

Vancouver:

Kumar SR. Sliding Mode Control Based Guidance Strategies with Terminal Constraints. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Dec 10]. 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


Indian Institute of Science

2. Ghosh, Satadal. Analysis of Proportional Navigation Class of Guidance Law against Agile Targets.

Degree: 2014, Indian Institute of Science

Guidance is defined as the determination of a strategy for following a nominal path in the presence of o-nominal conditions, disturbances and uncertainties, and the… (more)

Subjects/Keywords: Proportional Navigation; Maneuvering Target; Guidance; Augumented Pure Portional Navigation (APPN) Guidance Laws; Retro-PN Guidance Law; Guidance Laws; Higher-Speed Target; Agile Targets; Impact Angle Control; Composite Proportional Navigation (CPN); Impact Angle Analysis; Impact Time Control; Salvo Attack; Higher Speed Nonmaneuvering Targets; Time-varying Target; Mathematics

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

APA (6th Edition):

Ghosh, S. (2014). Analysis of Proportional Navigation Class of Guidance Law against Agile Targets. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2903

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):

Ghosh, Satadal. “Analysis of Proportional Navigation Class of Guidance Law against Agile Targets.” 2014. Thesis, Indian Institute of Science. Accessed December 10, 2019. http://hdl.handle.net/2005/2903.

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

MLA Handbook (7th Edition):

Ghosh, Satadal. “Analysis of Proportional Navigation Class of Guidance Law against Agile Targets.” 2014. Web. 10 Dec 2019.

Vancouver:

Ghosh S. Analysis of Proportional Navigation Class of Guidance Law against Agile Targets. [Internet] [Thesis]. Indian Institute of Science; 2014. [cited 2019 Dec 10]. Available from: http://hdl.handle.net/2005/2903.

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

Council of Science Editors:

Ghosh S. Analysis of Proportional Navigation Class of Guidance Law against Agile Targets. [Thesis]. Indian Institute of Science; 2014. Available from: http://hdl.handle.net/2005/2903

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

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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 10, 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. 10 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 10]. 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


Indian Institute of Science

4. Ratnoo, Ashwini. Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements.

Degree: 2009, Indian Institute of Science

 This thesis deals with development of guidance laws for advanced applications. Two class of guidance problems, namely, impact angle constrained guidance and pulsed guidance for… (more)

Subjects/Keywords: Guided Aircraft System; Guided Missile; Impact Angle Constraint; Exoatmospheric Constraint; Propotional Navigation Guidance (PNG) Law; State Dependent Riccati Equation Technique; Geometric Guidance Law; Exo-atmospheric Engagements; Pulsed Guidance Law; Lateral Impact; Impact Angle Constrained Trajectories; Military Engineering

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

APA (6th Edition):

Ratnoo, A. (2009). Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/929

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):

Ratnoo, Ashwini. “Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements.” 2009. Thesis, Indian Institute of Science. Accessed December 10, 2019. http://hdl.handle.net/2005/929.

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

MLA Handbook (7th Edition):

Ratnoo, Ashwini. “Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements.” 2009. Web. 10 Dec 2019.

Vancouver:

Ratnoo A. Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2019 Dec 10]. Available from: http://hdl.handle.net/2005/929.

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

Council of Science Editors:

Ratnoo A. Guidance Laws For Impact Angle Constraints And Exo-Atmospheric Engagements. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/929

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


Indian Institute of Science

5. Akhil, G. Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets.

Degree: 2017, Indian Institute of Science

 Various unmanned missions deploy vehicles such as missiles, torpedoes, ground robots, and unmanned aerial vehicles. Guidance strategies for these vehicles aim to intercept a target… (more)

Subjects/Keywords: Time-Optimal Guidance; Constrained Interception - Moving Targets; Relative Circular Navigation Guidance; Interception - Moving Targets; Impact Angle Constrained Guidance; Lateral Interception; Impact Angles; Maneuvering Targets; Time-optimal Impact Angle Constrained Paths; Optimal Paths; Dubins Paths; Aerospace Engineering

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

APA (6th Edition):

Akhil, G. (2017). Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3647 ; http://etd.iisc.ernet.in/abstracts/4517/G28472-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):

Akhil, G. “Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets.” 2017. Thesis, Indian Institute of Science. Accessed December 10, 2019. http://etd.iisc.ernet.in/2005/3647 ; http://etd.iisc.ernet.in/abstracts/4517/G28472-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):

Akhil, G. “Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets.” 2017. Web. 10 Dec 2019.

Vancouver:

Akhil G. Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets. [Internet] [Thesis]. Indian Institute of Science; 2017. [cited 2019 Dec 10]. Available from: http://etd.iisc.ernet.in/2005/3647 ; http://etd.iisc.ernet.in/abstracts/4517/G28472-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:

Akhil G. Time-Optimal Guidance for Impact Angle Constrained Interception of Moving Targets. [Thesis]. Indian Institute of Science; 2017. Available from: http://etd.iisc.ernet.in/2005/3647 ; http://etd.iisc.ernet.in/abstracts/4517/G28472-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

6. Bardhan, Rajarshi. Differential Games Guidance Laws for Aerospace Applications.

Degree: 2015, Indian Institute of Science

 This thesis addresses several aerospace guidance and decision making problems using both no cooperative and cooperative game theoretical solution concepts in the differential games framework.… (more)

Subjects/Keywords: Nonlinear Differential Games; Differential Games Guidance Law; Unmanned Aeial Vehicle (UAV); Maneuvering Target; State Dependent Riccati Equation (SDRE); Nash Bargaining Solution; UAVs; Unmanned Aeial Vehicles; Impact Angle Constrained Guidance; Rendezvous Gudance; Nonlinear Differential Guidance Law; Aerospace Engineering

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

APA (6th Edition):

Bardhan, R. (2015). Differential Games Guidance Laws for Aerospace Applications. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/2005/3889 ; http://etd.iisc.ernet.in/abstracts/4763/G27138-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):

Bardhan, Rajarshi. “Differential Games Guidance Laws for Aerospace Applications.” 2015. Thesis, Indian Institute of Science. Accessed December 10, 2019. http://etd.iisc.ernet.in/2005/3889 ; http://etd.iisc.ernet.in/abstracts/4763/G27138-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):

Bardhan, Rajarshi. “Differential Games Guidance Laws for Aerospace Applications.” 2015. Web. 10 Dec 2019.

Vancouver:

Bardhan R. Differential Games Guidance Laws for Aerospace Applications. [Internet] [Thesis]. Indian Institute of Science; 2015. [cited 2019 Dec 10]. Available from: http://etd.iisc.ernet.in/2005/3889 ; http://etd.iisc.ernet.in/abstracts/4763/G27138-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:

Bardhan R. Differential Games Guidance Laws for Aerospace Applications. [Thesis]. Indian Institute of Science; 2015. Available from: http://etd.iisc.ernet.in/2005/3889 ; http://etd.iisc.ernet.in/abstracts/4763/G27138-Abs.pdf

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

.