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You searched for +publisher:"Georgia Tech" +contributor:("Prasad, J. V. R."). Showing records 1 – 17 of 17 total matches.

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Georgia Tech

1. Park, Sang Gyun. Optimal control based method for design and analysis of continuous descent arrivals.

Degree: PhD, Aerospace Engineering, 2014, Georgia Tech

 Continuous Descent Arrival (CDA) is a procedure where aircraft descend, at or near idle thrust, from their cruise altitude to their Final Approach Fix without… (more)

Subjects/Keywords: Continuous descent arrival; Optimal control; Hybrid system; Trajectory optimization; Flight management system

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APA (6th Edition):

Park, S. G. (2014). Optimal control based method for design and analysis of continuous descent arrivals. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53005

Chicago Manual of Style (16th Edition):

Park, Sang Gyun. “Optimal control based method for design and analysis of continuous descent arrivals.” 2014. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/53005.

MLA Handbook (7th Edition):

Park, Sang Gyun. “Optimal control based method for design and analysis of continuous descent arrivals.” 2014. Web. 14 Apr 2021.

Vancouver:

Park SG. Optimal control based method for design and analysis of continuous descent arrivals. [Internet] [Doctoral dissertation]. Georgia Tech; 2014. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/53005.

Council of Science Editors:

Park SG. Optimal control based method for design and analysis of continuous descent arrivals. [Doctoral Dissertation]. Georgia Tech; 2014. Available from: http://hdl.handle.net/1853/53005


Georgia Tech

2. Zhou, Min. Trajectory optimization for fuel cell powered UAVs.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 This dissertation progressively addresses research problems related to the trajectory optimization for fuel cell powered UAVs, from propulsion system model development, to optimal trajectory analyses… (more)

Subjects/Keywords: Trajectory optimization; Fuel cell powered UAVs; Route planning; Optimal control; Drone aircraft; Fuel cell vehicles; Systems engineering; Aeronautics Systems engineering; Trajectories (Mechanics)

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APA (6th Edition):

Zhou, M. (2013). Trajectory optimization for fuel cell powered UAVs. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50235

Chicago Manual of Style (16th Edition):

Zhou, Min. “Trajectory optimization for fuel cell powered UAVs.” 2013. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/50235.

MLA Handbook (7th Edition):

Zhou, Min. “Trajectory optimization for fuel cell powered UAVs.” 2013. Web. 14 Apr 2021.

Vancouver:

Zhou M. Trajectory optimization for fuel cell powered UAVs. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/50235.

Council of Science Editors:

Zhou M. Trajectory optimization for fuel cell powered UAVs. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50235


Georgia Tech

3. Chung, Gi Yun. An analytical approach to real-time linearization of a gas turbine engine model.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 A recent development in the design of control system for a jet engine is to use a suitable, fast and accurate model running on board.… (more)

Subjects/Keywords: Analytical linearization, Real-time linearization; Off-equilibrium linearization; Off-equilibrium analytical linear model; Jet engine control; Gas turbine engine model based control; Control oriented model; Linear models (Statistics); Jet engines; Jet engines Control systems; Control theory

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APA (6th Edition):

Chung, G. Y. (2013). An analytical approach to real-time linearization of a gas turbine engine model. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50702

Chicago Manual of Style (16th Edition):

Chung, Gi Yun. “An analytical approach to real-time linearization of a gas turbine engine model.” 2013. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/50702.

MLA Handbook (7th Edition):

Chung, Gi Yun. “An analytical approach to real-time linearization of a gas turbine engine model.” 2013. Web. 14 Apr 2021.

Vancouver:

Chung GY. An analytical approach to real-time linearization of a gas turbine engine model. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/50702.

Council of Science Editors:

Chung GY. An analytical approach to real-time linearization of a gas turbine engine model. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50702


Georgia Tech

4. Kundu, Reema. Impact of engine icing on jet engine compressor flow dynamics.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Core engine icing has been recognized to affect a wide variety of engines since the 1990's. This previously unrecognized form of icing occurs in flights… (more)

Subjects/Keywords: Engine icing; Compressor; Jet engine; Compressible flow; Compressor stall

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APA (6th Edition):

Kundu, R. (2015). Impact of engine icing on jet engine compressor flow dynamics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54870

Chicago Manual of Style (16th Edition):

Kundu, Reema. “Impact of engine icing on jet engine compressor flow dynamics.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/54870.

MLA Handbook (7th Edition):

Kundu, Reema. “Impact of engine icing on jet engine compressor flow dynamics.” 2015. Web. 14 Apr 2021.

Vancouver:

Kundu R. Impact of engine icing on jet engine compressor flow dynamics. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/54870.

Council of Science Editors:

Kundu R. Impact of engine icing on jet engine compressor flow dynamics. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54870


Georgia Tech

5. Magree, Daniel Paul. Monocular vision-aided inertial navigation for unmanned aerial vehicles.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 The reliance of unmanned aerial vehicles (UAVs) on GPS and other external navigation aids has become a limiting factor for many missions. UAVs are now… (more)

Subjects/Keywords: Visual navigation; Filtering; Extended Kalman filter; Factorization methods; Unmanned aerial vehicles

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APA (6th Edition):

Magree, D. P. (2015). Monocular vision-aided inertial navigation for unmanned aerial vehicles. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53892

Chicago Manual of Style (16th Edition):

Magree, Daniel Paul. “Monocular vision-aided inertial navigation for unmanned aerial vehicles.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/53892.

MLA Handbook (7th Edition):

Magree, Daniel Paul. “Monocular vision-aided inertial navigation for unmanned aerial vehicles.” 2015. Web. 14 Apr 2021.

Vancouver:

Magree DP. Monocular vision-aided inertial navigation for unmanned aerial vehicles. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/53892.

Council of Science Editors:

Magree DP. Monocular vision-aided inertial navigation for unmanned aerial vehicles. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53892


Georgia Tech

6. Chandramohan, Rajeev. Output feedback adaptive control in the presence of unmodeled dynamics.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 This thesis outlines a method of output feedback adaptive control in the presence of matched unmodeled dynamics, uncertain control effectiveness and matched parametric uncertainties. An… (more)

Subjects/Keywords: Adaptive control; Output feedback; Flexible UAV; Unmodeled dynamics

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APA (6th Edition):

Chandramohan, R. (2016). Output feedback adaptive control in the presence of unmodeled dynamics. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/56285

Chicago Manual of Style (16th Edition):

Chandramohan, Rajeev. “Output feedback adaptive control in the presence of unmodeled dynamics.” 2016. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/56285.

MLA Handbook (7th Edition):

Chandramohan, Rajeev. “Output feedback adaptive control in the presence of unmodeled dynamics.” 2016. Web. 14 Apr 2021.

Vancouver:

Chandramohan R. Output feedback adaptive control in the presence of unmodeled dynamics. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/56285.

Council of Science Editors:

Chandramohan R. Output feedback adaptive control in the presence of unmodeled dynamics. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/56285

7. Kang, Keeryun. Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles.

Degree: PhD, Aerospace Engineering, 2012, Georgia Tech

 This thesis presents an integrated framework for online obstacle avoidance of rotary-wing unmanned aerial vehicles (UAVs), which can provide UAVs an obstacle field navigation capability… (more)

Subjects/Keywords: Real-time optimization; Trajectory optimization; UAV; Obstacle avoidance; Trajectory planning; Guidance systems (Flight); Drone aircraft; Flight control

…approximation of graphs . . . . . . . . . . . . . . . 108 58 UAV test-bed at Georgia Tech: The base… …Control Software GUST Georgia Tech UAV Simulation Tool INTOPTOA Integrated Optimal Obstacle… …framework is implemented in a real-time simulation environment, the Georgia Tech UAV Simulation… …test-bed at Georgia Tech. Initially, the 2D vertical avoidance capability of real obstacles… 

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APA (6th Edition):

Kang, K. (2012). Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/44820

Chicago Manual of Style (16th Edition):

Kang, Keeryun. “Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles.” 2012. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/44820.

MLA Handbook (7th Edition):

Kang, Keeryun. “Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles.” 2012. Web. 14 Apr 2021.

Vancouver:

Kang K. Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles. [Internet] [Doctoral dissertation]. Georgia Tech; 2012. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/44820.

Council of Science Editors:

Kang K. Online optimal obstacle avoidance for rotary-wing autonomous unmanned aerial vehicles. [Doctoral Dissertation]. Georgia Tech; 2012. Available from: http://hdl.handle.net/1853/44820

8. L'afflitto, Andrea. Finite-time partial stability, stabilization, semistabilization, and optimal feedback control.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Asymptotic stability is a key notion of system stability for controlled dynamical systems as it guarantees that the system trajectories are bounded in a neighborhood… (more)

Subjects/Keywords: Dynamic programming; Hamilton-Jacobi-Bellman; Optimal control; Finite-time stability; Partial-state stability; Partial-state finite-time stability; Stabilization; Feedback control; State-feedback control; Singular control

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APA (6th Edition):

L'afflitto, A. (2015). Finite-time partial stability, stabilization, semistabilization, and optimal feedback control. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53573

Chicago Manual of Style (16th Edition):

L'afflitto, Andrea. “Finite-time partial stability, stabilization, semistabilization, and optimal feedback control.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/53573.

MLA Handbook (7th Edition):

L'afflitto, Andrea. “Finite-time partial stability, stabilization, semistabilization, and optimal feedback control.” 2015. Web. 14 Apr 2021.

Vancouver:

L'afflitto A. Finite-time partial stability, stabilization, semistabilization, and optimal feedback control. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/53573.

Council of Science Editors:

L'afflitto A. Finite-time partial stability, stabilization, semistabilization, and optimal feedback control. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53573

9. Kim, Jee Woong. Development of a physics based methodology for the prediction of rotor blade ice formation.

Degree: PhD, Aerospace Engineering, 2015, Georgia Tech

 Modern helicopters, civilian and military alike, are expected to operate in all weather conditions. Ice accretion adversely affects the availability, affordability, safety and survivability. Availability… (more)

Subjects/Keywords: Rotorcraft; CFD; Icing; De-icing; Ice shedding

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APA (6th Edition):

Kim, J. W. (2015). Development of a physics based methodology for the prediction of rotor blade ice formation. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/54390

Chicago Manual of Style (16th Edition):

Kim, Jee Woong. “Development of a physics based methodology for the prediction of rotor blade ice formation.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/54390.

MLA Handbook (7th Edition):

Kim, Jee Woong. “Development of a physics based methodology for the prediction of rotor blade ice formation.” 2015. Web. 14 Apr 2021.

Vancouver:

Kim JW. Development of a physics based methodology for the prediction of rotor blade ice formation. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/54390.

Council of Science Editors:

Kim JW. Development of a physics based methodology for the prediction of rotor blade ice formation. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/54390

10. Sadikhov, Teymur. Stability, dissipativity, and optimal control of discontinuous dynamical systems.

Degree: Aerospace Engineering, 2015, Georgia Tech

 Discontinuous dynamical systems and multiagent systems are encountered in numerous engineering applications. This dissertation develops stability and dissipativity of nonlinear dynamical systems with discontinuous right-hand… (more)

Subjects/Keywords: Multiagent systems; Optimality; Dissipativity; Universal controller; Adaptive estimation; Sensor uncertainty; Set-valued analysis; Set-valued maps; Nonsmooth systems

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APA (6th Edition):

Sadikhov, T. (2015). Stability, dissipativity, and optimal control of discontinuous dynamical systems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/53635

Chicago Manual of Style (16th Edition):

Sadikhov, Teymur. “Stability, dissipativity, and optimal control of discontinuous dynamical systems.” 2015. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/53635.

MLA Handbook (7th Edition):

Sadikhov, Teymur. “Stability, dissipativity, and optimal control of discontinuous dynamical systems.” 2015. Web. 14 Apr 2021.

Vancouver:

Sadikhov T. Stability, dissipativity, and optimal control of discontinuous dynamical systems. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/53635.

Council of Science Editors:

Sadikhov T. Stability, dissipativity, and optimal control of discontinuous dynamical systems. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/53635

11. Valenzuela-Del Rio, Jose Eugenio. Bayesian adaptive sampling for discrete design alternatives in conceptual design.

Degree: PhD, Aerospace Engineering, 2013, Georgia Tech

 The number of technology alternatives has lately grown to satisfy the increasingly demanding goals in modern engineering. These technology alternatives are handled in the design… (more)

Subjects/Keywords: Design alternatives; Conceptual design; Surrogates; Adaptive sampling; Concept; Categories; Mixed-integer optimization; Multi-fidelity; Kriging; Multi-objective; Helicopter; Systems engineering; Simulation methods; Concepts; Adaptive sampling (Statistics); Algorithms; Genetic algorithms

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APA (6th Edition):

Valenzuela-Del Rio, J. E. (2013). Bayesian adaptive sampling for discrete design alternatives in conceptual design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/50263

Chicago Manual of Style (16th Edition):

Valenzuela-Del Rio, Jose Eugenio. “Bayesian adaptive sampling for discrete design alternatives in conceptual design.” 2013. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/50263.

MLA Handbook (7th Edition):

Valenzuela-Del Rio, Jose Eugenio. “Bayesian adaptive sampling for discrete design alternatives in conceptual design.” 2013. Web. 14 Apr 2021.

Vancouver:

Valenzuela-Del Rio JE. Bayesian adaptive sampling for discrete design alternatives in conceptual design. [Internet] [Doctoral dissertation]. Georgia Tech; 2013. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/50263.

Council of Science Editors:

Valenzuela-Del Rio JE. Bayesian adaptive sampling for discrete design alternatives in conceptual design. [Doctoral Dissertation]. Georgia Tech; 2013. Available from: http://hdl.handle.net/1853/50263

12. Gavrilovski, Alek. Predictive helicopter flight data monitoring for flight safety design.

Degree: PhD, Aerospace Engineering, 2017, Georgia Tech

 A method to augment existing Helicopter Flight Data Monitoring (HFDM) systems using physics-based models was proposed. It was suggested that physics-based models can be utilized… (more)

Subjects/Keywords: Rotorcraft; Helicopter; Flight data recorder; Safety; Flight data monitoring; Dynamics; Simulations; Safety database; Prognostics and health monitoring; PHM

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APA (6th Edition):

Gavrilovski, A. (2017). Predictive helicopter flight data monitoring for flight safety design. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/58227

Chicago Manual of Style (16th Edition):

Gavrilovski, Alek. “Predictive helicopter flight data monitoring for flight safety design.” 2017. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/58227.

MLA Handbook (7th Edition):

Gavrilovski, Alek. “Predictive helicopter flight data monitoring for flight safety design.” 2017. Web. 14 Apr 2021.

Vancouver:

Gavrilovski A. Predictive helicopter flight data monitoring for flight safety design. [Internet] [Doctoral dissertation]. Georgia Tech; 2017. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/58227.

Council of Science Editors:

Gavrilovski A. Predictive helicopter flight data monitoring for flight safety design. [Doctoral Dissertation]. Georgia Tech; 2017. Available from: http://hdl.handle.net/1853/58227

13. Rajpurohit, Tanmay. Stochastic nonlinear control: A unified framework for stability, dissipativity, and optimality.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 In this work, we develop connections between stochastic stability theory and stochastic optimal control. In particular, first we develop Lyapunov and converse Lyapunov theorems for… (more)

Subjects/Keywords: Stochastic dissipativity; Markov diffusion processes; Extended Kalman-Yakubovich-Popov conditions; Stochastic stability of feedback systems; Stochastic semistability; Lyapunov theory; Converse Lyapunov theorems; Stochastic finite-time stability; Partial stochastic stability; Finite-time stabilization; Partial-state stabilization; Lyapunov differential inequalities; Stochastic optimal control; Stochastic Hamilton-Jacobi-Bellman theory; Time-varying systems; Stochastic differential games; Inverse optimal control; Stochastic Hamilton-Jacobi-Isaacs equation; Polynomial cost functions; Multilinear forms

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APA (6th Edition):

Rajpurohit, T. (2018). Stochastic nonlinear control: A unified framework for stability, dissipativity, and optimality. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/59856

Chicago Manual of Style (16th Edition):

Rajpurohit, Tanmay. “Stochastic nonlinear control: A unified framework for stability, dissipativity, and optimality.” 2018. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/59856.

MLA Handbook (7th Edition):

Rajpurohit, Tanmay. “Stochastic nonlinear control: A unified framework for stability, dissipativity, and optimality.” 2018. Web. 14 Apr 2021.

Vancouver:

Rajpurohit T. Stochastic nonlinear control: A unified framework for stability, dissipativity, and optimality. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/59856.

Council of Science Editors:

Rajpurohit T. Stochastic nonlinear control: A unified framework for stability, dissipativity, and optimality. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/59856

14. Lopez, Mark Joseph Santos. Linear time invariant approximations of linear time periodic systems for integrated flight and vibration control.

Degree: PhD, Aerospace Engineering, 2016, Georgia Tech

 Recent developments in active rotor control have shown significant coupling between flight and vibration control systems which are traditionally designed independently. This coupling results in… (more)

Subjects/Keywords: Rotorcraft; Linear time invariant models; Integrated flight and vibration control

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APA (6th Edition):

Lopez, M. J. S. (2016). Linear time invariant approximations of linear time periodic systems for integrated flight and vibration control. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55599

Chicago Manual of Style (16th Edition):

Lopez, Mark Joseph Santos. “Linear time invariant approximations of linear time periodic systems for integrated flight and vibration control.” 2016. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/55599.

MLA Handbook (7th Edition):

Lopez, Mark Joseph Santos. “Linear time invariant approximations of linear time periodic systems for integrated flight and vibration control.” 2016. Web. 14 Apr 2021.

Vancouver:

Lopez MJS. Linear time invariant approximations of linear time periodic systems for integrated flight and vibration control. [Internet] [Doctoral dissertation]. Georgia Tech; 2016. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/55599.

Council of Science Editors:

Lopez MJS. Linear time invariant approximations of linear time periodic systems for integrated flight and vibration control. [Doctoral Dissertation]. Georgia Tech; 2016. Available from: http://hdl.handle.net/1853/55599


Georgia Tech

15. Yoon, Hyungjoo. Spacecraft Attitude and Power Control Using Variable Speed Control Moment Gyros.

Degree: PhD, Aerospace Engineering, 2004, Georgia Tech

 A Variable Speed Control Moment Gyro (VSCMG) is a recently introduced actuator for spacecraft attitude control. As its name implies, a VSCMG is essentially a… (more)

Subjects/Keywords: Mechanical battery; Singularity avoidance; Attitude control; IPACS; Control moment gyro; VSCMG; Space vehicles Dynamics; Space vehicles Control systems; Automatic control; Astrodynamics; Actuators

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APA (6th Edition):

Yoon, H. (2004). Spacecraft Attitude and Power Control Using Variable Speed Control Moment Gyros. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/4850

Chicago Manual of Style (16th Edition):

Yoon, Hyungjoo. “Spacecraft Attitude and Power Control Using Variable Speed Control Moment Gyros.” 2004. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/4850.

MLA Handbook (7th Edition):

Yoon, Hyungjoo. “Spacecraft Attitude and Power Control Using Variable Speed Control Moment Gyros.” 2004. Web. 14 Apr 2021.

Vancouver:

Yoon H. Spacecraft Attitude and Power Control Using Variable Speed Control Moment Gyros. [Internet] [Doctoral dissertation]. Georgia Tech; 2004. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/4850.

Council of Science Editors:

Yoon H. Spacecraft Attitude and Power Control Using Variable Speed Control Moment Gyros. [Doctoral Dissertation]. Georgia Tech; 2004. Available from: http://hdl.handle.net/1853/4850


Georgia Tech

16. Cordeiro, Helio de Miranda. Stochastic dynamical system identification applied to combustor stability margin assessment.

Degree: PhD, Aerospace Engineering, 2008, Georgia Tech

 A new approach was developed to determine the operational stability margin of a laboratory scale combustor. Applying modern and robust techniques and tools from Dynamical… (more)

Subjects/Keywords: System identification; Stability margin; Combustion instability; Combustion engineering; Acoustical engineering; Thermodynamics; Combustion chambers

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APA (6th Edition):

Cordeiro, H. d. M. (2008). Stochastic dynamical system identification applied to combustor stability margin assessment. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/28167

Chicago Manual of Style (16th Edition):

Cordeiro, Helio de Miranda. “Stochastic dynamical system identification applied to combustor stability margin assessment.” 2008. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/28167.

MLA Handbook (7th Edition):

Cordeiro, Helio de Miranda. “Stochastic dynamical system identification applied to combustor stability margin assessment.” 2008. Web. 14 Apr 2021.

Vancouver:

Cordeiro HdM. Stochastic dynamical system identification applied to combustor stability margin assessment. [Internet] [Doctoral dissertation]. Georgia Tech; 2008. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/28167.

Council of Science Editors:

Cordeiro HdM. Stochastic dynamical system identification applied to combustor stability margin assessment. [Doctoral Dissertation]. Georgia Tech; 2008. Available from: http://hdl.handle.net/1853/28167


Georgia Tech

17. Jain, Sachin. Multiresolution strategies for the numerical solution of optimal control problems.

Degree: PhD, Aerospace Engineering, 2008, Georgia Tech

 Optimal control problems are often characterized by discontinuities or switchings in the control variables. One way of accurately capturing the irregularities in the solution is… (more)

Subjects/Keywords: Mesh refinement; Multiresolution; Optimal control; Evolution pdes; Control theory; Mathematical optimization; Data compression (Computer science); Numerical grid generation (Numerical analysis); Algorithms

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APA (6th Edition):

Jain, S. (2008). Multiresolution strategies for the numerical solution of optimal control problems. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/22656

Chicago Manual of Style (16th Edition):

Jain, Sachin. “Multiresolution strategies for the numerical solution of optimal control problems.” 2008. Doctoral Dissertation, Georgia Tech. Accessed April 14, 2021. http://hdl.handle.net/1853/22656.

MLA Handbook (7th Edition):

Jain, Sachin. “Multiresolution strategies for the numerical solution of optimal control problems.” 2008. Web. 14 Apr 2021.

Vancouver:

Jain S. Multiresolution strategies for the numerical solution of optimal control problems. [Internet] [Doctoral dissertation]. Georgia Tech; 2008. [cited 2021 Apr 14]. Available from: http://hdl.handle.net/1853/22656.

Council of Science Editors:

Jain S. Multiresolution strategies for the numerical solution of optimal control problems. [Doctoral Dissertation]. Georgia Tech; 2008. Available from: http://hdl.handle.net/1853/22656

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