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Relook at Aileron to Rudder Interconnect

Defense science journal, 2021-03, Vol.71 (2), p.153-161

2021

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L1 adaptive controller for tailless unstable aircraft in the presence of unknown actuator failures

International journal of control, 2009-04, Vol.82 (4), p.705-720

2009

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Guaranteed Stability of Polynomials Under Application of a Uniform Nonnegative Polynomial Mapping on Coefficients

IEEE transactions on automatic control, 2009-06, Vol.54 (6), p.1311-1313

2009

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Autonomous Landing Design of UAVs using Feedback Linearization Controller with Anti Windup Scheme

IFAC-PapersOnLine, 2020, Vol.53 (1), p.81-86

2020

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Autonomous Landing of Fixed Wing Unmanned Aerial Vehicle with Reactive Collision Avoidance

IFAC-PapersOnLine, 2018, Vol.51 (1), p.474-479

2018

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Some applications of randomized algorithms for control system design

Automatica (Oxford), 2002-12, Vol.38 (12), p.2085-2092

2002

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Reliable Fault Identification for Aircraft Control Surface Damage

2019 Sixth Indian Control Conference (ICC), 2019, p.490-495

2019

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Partially Structured LQR design for Lateral-Directional Flight Control Law

2019 Innovations in Power and Advanced Computing Technologies (i-PACT), 2019, Vol.1, p.1-6

2019

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Accelerated Flight Control LAW Clearance Using Stores Grouping Concept

IFAC-PapersOnLine, 2018, Vol.51 (1), p.365-370

2018

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A Detail of Fault Tolerant Flight Control Techniques

International journal of recent technology and engineering, 2020-05, Vol.9 (1), p.617-625

2020

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Vision Based Automatic Landing with Runway Identification and Tracking

2018 15th International Conference on Control, Automation, Robotics and Vision (ICARCV), 2018, p.1442-1447

2018

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Advanced Distributed Flight Control System Architecture with Prognosis for High Performance Fighter Aircraft

International journal of engineering trends and technology, 2016-12, Vol.42 (8), p.416-420

2016

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Design of Notch Filters for Structural Responses with Multiaxis Coupling

Journal of guidance, control, and dynamics, 1999-03, Vol.22 (2), p.349-357

1999

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Vision Based Runway Identification with marked or unmarked terrain for Automatic Landing Applications of UAV

IFAC-PapersOnLine, 2024, Vol.57, p.125-130

2024

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Pitch and roll angle estimation using partial DCM model approach for a high performance aircraft

2016 Indian Control Conference (ICC), 2016, p.312-317

2016

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Real-Time Vision-Based Aircraft Vertical Tail Damage Detection and Parameter Estimation

Journal of the Institution of Electronics and Telecommunication Engineers, 2023-11, Vol.69 (11), p.8193-8204

2023

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ℒ 1 adaptive controller for tailless unstable aircraft in the presence of unknown actuator failures

International journal of control, 2009-04, Vol.82 (4), p.705-720

2009

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Autonomous Landing of UAVs with Reactive Collision Avoidance using Mixed Guidance Scheme and Neuro Adaptive Controller

2021 International Symposium of Asian Control Association on Intelligent Robotics and Industrial Automation (IRIA), 2021, p.364-369

2021

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Autonomous Landing for Small UAVs using L Adaptive Control Tracking Applications

2019 Fifth Indian Control Conference (ICC), 2019, p.472-477

2019

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Autonomous Landing of UAVs under Unknown Disturbances using NDI Autopilot with L 1 Adaptive Augmentation

IFAC-PapersOnLine, 2017-07, Vol.50 (1), p.3680-3684

2017

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Perfecting Handling Qualities Assessment Task on Simulator and Outcome of Actual Flight Test for Air to Air Refueling

2019 Sixth Indian Control Conference (ICC), 2019, p.473-478

2019

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Development and Flight Testing of an Automatic Leveling Function for a Fighter Aircraft

IFAC-PapersOnLine, 2018, Vol.51 (1), p.359-364

2018

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Solution to the “Champagne problem” on the simultaneous stabilisation of three plants

Systems & control letters, 1999, Vol.37 (3), p.173-175

Patel, Vijay V.

1999

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On Multiple Interpolation Points of H∞-Units at Infinity

Journal of the Institution of Electronics and Telecommunication Engineers, 1999-03, Vol.45 (2), p.113-114

1999

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Robust Optimal Controller for a Helicopter Model

Journal of the Institution of Electronics and Telecommunication Engineers, 1999-03, Vol.45 (2), p.103-112

1999

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Relook at Aileron to Rudder Interconnect

L1 adaptive controller for tailless unstable aircraft in the presence of unknown actuator failures

Guaranteed Stability of Polynomials Under Application of a Uniform Nonnegative Polynomial Mapping on Coefficients

Autonomous Landing Design of UAVs using Feedback Linearization Controller with Anti Windup Scheme

Autonomous Landing of Fixed Wing Unmanned Aerial Vehicle with Reactive Collision Avoidance

Some applications of randomized algorithms for control system design

Reliable Fault Identification for Aircraft Control Surface Damage

Partially Structured LQR design for Lateral-Directional Flight Control Law

Accelerated Flight Control LAW Clearance Using Stores Grouping Concept

A Detail of Fault Tolerant Flight Control Techniques

Vision Based Automatic Landing with Runway Identification and Tracking

Advanced Distributed Flight Control System Architecture with Prognosis for High Performance Fighter Aircraft

Design of Notch Filters for Structural Responses with Multiaxis Coupling

Vision Based Runway Identification with marked or unmarked terrain for Automatic Landing Applications of UAV

Pitch and roll angle estimation using partial DCM model approach for a high performance aircraft

Real-Time Vision-Based Aircraft Vertical Tail Damage Detection and Parameter Estimation

ℒ 1 adaptive controller for tailless unstable aircraft in the presence of unknown actuator failures

Autonomous Landing of UAVs with Reactive Collision Avoidance using Mixed Guidance Scheme and Neuro Adaptive Controller

Autonomous Landing for Small UAVs using L Adaptive Control Tracking Applications

Autonomous Landing of UAVs under Unknown Disturbances using NDI Autopilot with L 1 Adaptive Augmentation

Perfecting Handling Qualities Assessment Task on Simulator and Outcome of Actual Flight Test for Air to Air Refueling

Development and Flight Testing of an Automatic Leveling Function for a Fighter Aircraft

Solution to the “Champagne problem” on the simultaneous stabilisation of three plants

On Multiple Interpolation Points of H∞-Units at Infinity

Robust Optimal Controller for a Helicopter Model

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