FLIGHT MECHANICS AND CONTROL DIVISION

Flight Mechanics & Control Division is one of NAL’s leading departments that has played a stellar role in providing technology solutions to major aviation and aerospace programs in the country.

The division has a high level of expertise in Flight Simulation, Control and Handling Qualities, Aircraft System Identification, Multi Sensor Data Fusion and Unmanned Air Systems. 

 

Control & Handling Qualities Group & the National CLAW Team

The National Control Law Team, that comprises of the best talent from FMCD, ADA, CAIR, and HAL operates from the premises of FMCD. The team has made a major contribution in the design and development of the complex fly-by-wire flight control system of India’s Light Combat Aircraft.

More than twenty test pilots have flown LCA-Tejas and have applauded the team for delivering an aircraft with excellent handling qualities and capabilities. Today, Tejas compares with the best fighter aircrafts in the world with features such as boundary limiting, automatic low speed recovery and carefree maneuvering.

Its state-of-the-art autopilot supports altitude and flight path select & hold mode, as well as auto level features with both horizontal and vertical navigation modes. The sophisticated control-laws are devised to permit Air-to-Air refueling  as well as carriage and release of a range of weapons from the aircraft.

The team has successfully designed air data algorithms to ensure accurate measurement of flow angles and pressure probe readings.

A stiff challenge for the team was to design the flight control laws of LCA Naval variant for short take-off from a ship deck and arrestor-hook landing. A special hands-free takeoff mode was developed to overcome the constraints of the short runway.

The flawless flying demonstrations of LCA-Tejas at Aero India Bangalore and Bahrain Airshow amply demonstrate the team’s expertise and capabilities in flight control design.

 

Flight Simulation Group

The Flight simulator designed at FMCD has been instrumental in validation and final implementation of LCA’s control design. This  high-fidelity real-time simulator  provides high quality visual cues to LCA pilots.

Special scenarios can be created to familiarize the pilots with turbulence, crosswinds, take-off from ship deck, landing with arrestor-hook, air-to-air refueling and auto low speed recovery.

FMCD team has also developed several other simulators, including desktop simulators for engineering students and Handling Qualities simulator for the Air Force Test Pilot School.

A multifunctional simulator has been developed for CSIR-NAL’s 14 Seater, SARAS Aircraft, to provide cockpit and procedure familiarization to pilots. A head & eye tracking system is also installed to measure pilot workload.

 

An Augmented Engineering Environment Simulator was designed jointly with CAE Canada, for studies in aircraft design validation, cockpit ergonomics, Pilot Vehicle Interface and Hazard analysis. A dedicated simulator of Advanced Medium Combat Aircraft (AMCA), was built by FMCD to assist ADA for evaluating controller design and avionics displays for this fifth-generation fighter aircraft.

The team also has expertise in the area of Air Traffic Management. Airport capacity studies, noise prediction, air traffic controller work load assessment and fuel burn studies have been executed using this facility.

 

 

Aircraft System Identification Group

A key requirement for aircraft control design is the availability of accurate aerodynamic models. This requires a coordinated approach using flight data gathering, mathematical modeling and advanced system identification tools.

 

FMCD has mastered these highly sophisticated technologies that are closely guarded by the leading aerospace agencies in the world. The team has rich experience in model identification from flight data.  The identified models are used to improve simulator fidelity, to evaluate aircraft performance and for upgrading flight control laws.

 

The team has contributed immensely to the safe and systematic expansion of LCA-Tejas flight envelope. The team has also analyzed flight data from several other aircraft, including SARAS, MIG-21, Jaguar, Advanced Light Helicopter and unmanned air vehicles.

The division has  made significant contributions to several other vital projects, such as flight clearance of stores for mid-life up-gradation of the Mirage 2000 aircraft. 

 

 

Multi Sensor Data Fusion Group

 

FMCD’s expertise extends beyond aircraft control design to the complex area of multi-sensor data fusion.

The expert group working in this area has developed target tracking algorithms for the integrated test range facility of DRDO.  Sophisticated algorithms were also developed for C4I National Air Defense Programme.

Seeker filter algorithms were developed for ASTRA air-to-air missiles to intercept highly maneuvering air breathing targets. An automatic threat assessment system was developed to improve pilot’s situational awareness and to reduce his workload in combat situations.

The expert group is currently developing an advanced cockpit display technology, called ‘Enhanced synthetic vision system’, to enable pilots to perform safe flight operations in reduced visibility conditions.

 

This technology will enable flight operations in all weather conditions from any airport, including ones that are not well-equipped for low visibility operations.

 

MAV UNIT

 

FMCD has also been contributing to the development of unmanned air systems at NAL.

The division is actively supporting the MAV unit of CSIR-NAL, which provides the lead in the design and fabrication of fully indigenized mini air vehicles.

FMCD team has been instrumental in developing the flight control algorithms and hardware-in-Loop simulation for the MAV program. The division also assists MAV unit in vehicle integration and flight testing activities.

 

 

International Collaborations

FMCD has been involved in several collaborative programs with international agencies like DLR Institute of Flight Systems, Germany, De-Montfort University in Leicester, UK and CAE, Canada.

 

Concluding Remarks

 

As the division looks to make foray into the new challenging areas of Aerospace sector, it is open to scientific and technical collaborations, industrial partnerships, transfer of technology and joint development with Indian and Foreign partners.

 

With its unparalleled expertise in the areas of flight control design, simulation, system identification and data fusion, FMCD will continue to deliver critical technologies to the various aerospace programs that the country may plan to undertake in the times to come.

HEAD

JATINDER SINGH

DEPUTY HEAD

LATHASREE P

CHIEF SCIENTIST

SINGH G K

SENIOR PRINCIPAL SCIENTIST (5)

KAMALI C DR
NAIDU V P S DR
SRIKANTH K P
SUDESH KUMAR KASHYAP
KUMARESAN G

PRINCIPAL SCIENTIST (5)

ARCHANA HEBBAR P
DEVENDRA SINGH
GURUGANESH R
KHADEEJA NUSRATH T K
VISWANATHAN S

SENIOR SCIENTIST (4)

ALEXANDER KALE
SANKETH AILNENI
SHRI NAVENDU KUMAR
DUSHYANT KALIYARI

TECHNICAL STAFF (4)

Vijeesh T
Hanumantha
Vimalraj A
Mahesh

TECHNIQUES

JATINDER SINGH

Dr Jatinder has been extensively involved in aircraft modeling and parameter estimation work and has made significant contribution to the LCA program…

More

JATINDER SINGH is working on Techniques

JATINDER SINGH is working on Facilities

VISWANATHAN S

Viswanathan S  completed his B.E in Aeronautical Engineering from Bharathiyar University in 2004. He completed his Master’s degree in Aerospace…

More

VISWANATHAN S is working on Techniques

VISWANATHAN S is working on Facilities

KHADEEJA NUSRATH T K

Khadeeja Nusrath TK has been extensively involved in aircraft system identification and parameter estimation.  Her specific focus areas are flight…

More

KHADEEJA NUSRATH T K is working on Techniques

KHADEEJA NUSRATH T K is working on Facilities

GURUGANESH R

Guruganesh has been working in the area of design, developemnt, verification and testing of flight control laws for various classes of aircraft…

More

GURUGANESH R is working on Techniques

GURUGANESH R is working on Facilities

DEVENDRA SINGH

Devendra’s research is concerned with aircraft design, performance and flight mechanics. Particular focus areas are theoretical computation of…

More

DEVENDRA SINGH is working on Techniques

DEVENDRA SINGH is working on Facilities

ARCHANA HEBBAR P

Archana Hebbar’s research interests include flight simulations, pilot workload assessment and Human machine interface design. Her research is…

More

ARCHANA HEBBAR P is working on Techniques

ARCHANA HEBBAR P is working on Facilities

DUSHYANT KALIYARI

Dushyant Kaliyari, a graduate of Bhilai Institute of Technology Durg (2011) with a degree in Electronics & Telecommunication and a masters in…

More

DUSHYANT KALIYARI is working on Techniques

DUSHYANT KALIYARI is working on Facilities

SHRI NAVENDU KUMAR

My research activities are primarily connected to the development of generic Flight Simulator (Civil/Military). I carried out the following…

More

SHRI NAVENDU KUMAR is working on Techniques

SHRI NAVENDU KUMAR is working on Facilities

SANKETH AILNENI

Sanketh Ailneni has a Masters in Aerospace Engineering from Academy of Scientific & Industrial Research (AcSIR – NAL), Bangalore. Presently he is…

More

SANKETH AILNENI is working on Techniques

SANKETH AILNENI is working on Facilities

ALEXANDER KALE

His research area include guidance and control of fixedwing and multirotor MAV/UAVs, adaptive and classical control with applications to aerospace…

More

ALEXANDER KALE is working on Techniques

ALEXANDER KALE is working on Facilities

Mahesh is working on Techniques

Mahesh is working on Facilities

Vijeesh T is working on Techniques

Vijeesh T is working on Facilities

Hanumantha is working on Techniques

Hanumantha is working on Facilities

Vimalraj A is working on Techniques

Vimalraj A is working on Facilities

LATHASREE P

 Lathasree’s research is concerned with flight mechanics and control, particularly for fixed wing aircraft. She has significantly contributed towards…

More

LATHASREE P is working on Techniques

LATHASREE P is working on Facilities

KUMARESAN G

Kumaresan’s research area include flight control, adaptive control and multi agent control with application to aerospace vehicles. Recent focus is on…

More

KUMARESAN G is working on Techniques

KUMARESAN G is working on Facilities

SRIKANTH K P

He has a Master’s degree in Software Engineering from BITS, Pilani (1995). He joined NAL in Dec 1996 as Scientist B. He working areas are Flight…

More

SRIKANTH K P is working on Techniques

SRIKANTH K P is working on Facilities

NAIDU V P S DR

His research is concerned with fundamental and applied research in the area of multi-sensor data fusion and state estimation. Particular focus areas…

More

NAIDU V P S DR is working on Techniques

NAIDU V P S DR is working on Facilities

KAMALI C DR

Kamali’s research is concerned with flight simulation, navigation, parameter estimation and airdata calibration. Works for national projects such as…

More

KAMALI C DR is working on Techniques

KAMALI C DR is working on Facilities

SINGH G K

G.K. Singh has been working in the Flight Mechanics & Control Division of CSIR-NAL since 1998.  He has been involved in the design, development,…

More

SINGH G K is working on Techniques

SINGH G K is working on Facilities

MULTI AGENT COOPERATIVE CONTROL PROCESSOR-IN-THE LOOP (PIL) FACILITY

MULTI AGENT COOPERATIVE CONTROL PROCESSOR-IN-THE LOOP (PIL) FACILITY

Multi agent Cooperative Control Processor-in-the Loop (PIL) Facility

  • Established the formation flying Processor -in-the Loop (PIL) to test formation flying of

More

SCIENTISTS WORKING ON MULTI AGENT COOPERATIVE CONTROL PROCESSOR-IN-THE LOOP (PIL) FACILITY

MODEL BASED DESIGN APPROACH: MAV AUTOPILOT FUNCTIONALITY DESIGN

MODEL BASED DESIGN APPROACH: MAV AUTOPILOT FUNCTIONALITY DESIGN

Model based design approach: MAV autopilot functionality design

Model based design framework is getting popular in the aerospace sector for flight control applications.

More

SCIENTISTS WORKING ON MODEL BASED DESIGN APPROACH: MAV AUTOPILOT FUNCTIONALITY DESIGN

L1 ADAPTIVE CONTROL WITH APPLICATIONS TO AEROSPACE VEHICLES

L1 ADAPTIVE CONTROL WITH APPLICATIONS TO AEROSPACE VEHICLES

L1 adaptive control with applications to aerospace vehicles

Longitudinal flight control system designed based on total energy control system (TECS) using ℒ1 adaptive cont

More

SCIENTISTS WORKING ON L1 ADAPTIVE CONTROL WITH APPLICATIONS TO AEROSPACE VEHICLES

AIRCRAFT SYSTEM MODELING AND SIMULATION

AIRCRAFT SYSTEM MODELING AND SIMULATION

Aircraft system modeling and simulation

An aircraft simulation model consists of several sub system models for 6 DOF flight dynamics, engine, fuel, sensors, landing gear,

More

SCIENTISTS WORKING ON AIRCRAFT SYSTEM MODELING AND SIMULATION

SIMULATION BASED VIRTUAL REALITY

SIMULATION BASED VIRTUAL REALITY

Simulation based Virtual Reality

The method of virtual reality for aircraft simulation provides the required cues for the pilot to feel the dynamics of the modeled aircra

More

SCIENTISTS WORKING ON SIMULATION BASED VIRTUAL REALITY

STATISTICAL TOOLS AND TECHNIQUES FOR PILOT WORKLOAD ASSESSMENT

STATISTICAL TOOLS AND TECHNIQUES FOR PILOT WORKLOAD ASSESSMENT

Statistical tools and techniques for pilot workload assessment

Research studies are carried out on human factor issues in an aircraft program such as pilot’s mental workl

More

SCIENTISTS WORKING ON STATISTICAL TOOLS AND TECHNIQUES FOR PILOT WORKLOAD ASSESSMENT

USER INTERFACE DESIGN USING VISUAL C++ PROGRAMMING

USER INTERFACE DESIGN USING VISUAL C++ PROGRAMMING

User Interface design using Visual C++ programming

One of the main systems in a flight simulator is the ‘Instructor station’.

More

SCIENTISTS WORKING ON USER INTERFACE DESIGN USING VISUAL C++ PROGRAMMING

EMPIRICAL ESTIMATION OF AERO-DATA AND PERFORMANCE PARAMETERS

EMPIRICAL ESTIMATION OF AERO-DATA AND PERFORMANCE PARAMETERS

Empirical estimation of aero-data and performance parameters

Based of theoretical concept MATLAB based scripts have been used for aero-data and performance parameters est

More

SCIENTISTS WORKING ON EMPIRICAL ESTIMATION OF AERO-DATA AND PERFORMANCE PARAMETERS

PARAMETER ESTIMATION TECHNIQUES IN TIME DOMAIN AND FREQUENCY DOMAIN

PARAMETER ESTIMATION TECHNIQUES IN TIME DOMAIN AND FREQUENCY DOMAIN

Parameter Estimation Techniques in time domain and frequency domain

Output Error Method, Filter Error method, Extended Kalman Filter, Feed Forward Neural Networks and Dis

More

SCIENTISTS WORKING ON PARAMETER ESTIMATION TECHNIQUES IN TIME DOMAIN AND FREQUENCY DOMAIN

SLIDING MODE CONTROL TECHNIQUES FOR MICRO AERIAL VEHICLES

SLIDING MODE CONTROL TECHNIQUES FOR MICRO AERIAL VEHICLES

Sliding mode control techniques for Micro Aerial Vehicles

Advancement in Sliding mode control (SMC) in the past few decades has helped researchers in solving many interes

More

SCIENTISTS WORKING ON SLIDING MODE CONTROL TECHNIQUES FOR MICRO AERIAL VEHICLES

MODELING AND SIMULATION

MODELING AND SIMULATION

Modeling and Simulation

Modelling and simulation techniques are used in all the flight simulator facilities mentioned.

More

SCIENTISTS WORKING ON MODELING AND SIMULATION

REAL TIME PARAMETER ESTIMATION

REAL TIME PARAMETER ESTIMATION

Real time parameter estimation

Developed algorithms for real time parameter estimation of aircraft.

More

SCIENTISTS WORKING ON REAL TIME PARAMETER ESTIMATION

FLUSH AIRDATA SYSTEM (FADS) ALGORITHMS:

FLUSH AIRDATA SYSTEM (FADS) ALGORITHMS:

Flush AirData System (FADS) Algorithms:

Presently developing algorithms for FADS. The algorithm is proven on CFD data in a 6 DOF simulation platform.

More

SCIENTISTS WORKING ON FLUSH AIRDATA SYSTEM (FADS) ALGORITHMS:

EKF BASED ALGORITHMS FOR INS/GPS FUSION FOR UAVS

EKF BASED ALGORITHMS FOR INS/GPS FUSION FOR UAVS

EKF based algorithms for INS/GPS fusion for UAVs

The design of an EKF is addressed for the purpose of estimating the position, velocity, attitude and heading of an Aircra

More

SCIENTISTS WORKING ON EKF BASED ALGORITHMS FOR INS/GPS FUSION FOR UAVS

EKF BASED ALGORITHMS FOR ATTITUDE AND HEADING ESTIMATION OF UAV

EKF BASED ALGORITHMS FOR ATTITUDE AND HEADING ESTIMATION OF UAV

EKF based algorithms for attitude and Heading estimation of UAV

Extended Kalman filter (EKF) solution for attitude and heading estimation was proposed with code phase GPS

More

SCIENTISTS WORKING ON EKF BASED ALGORITHMS FOR ATTITUDE AND HEADING ESTIMATION OF UAV

AIRDATA CALIBRATION AND ACCURACY DETERMINATION

AIRDATA CALIBRATION AND ACCURACY DETERMINATION

Airdata calibration and accuracy determination

An Air Data System (ADS) plays a key role in stabilization, control and improving performance of modern fighter aircraft.

More

SCIENTISTS WORKING ON AIRDATA CALIBRATION AND ACCURACY DETERMINATION

PURSUIT BASED GUIDANCE CONTROL, L-PSI CONTROL, LQR FORMATION CONTROL AND L1 ADAPTIVE CONTROL FOR THE CONTROL OF MULTI AGENT SYSTEM

PURSUIT BASED GUIDANCE CONTROL, L-PSI CONTROL, LQR FORMATION CONTROL AND L1 ADAPTIVE CONTROL FOR THE CONTROL OF MULTI AGENT SYSTEM

pursuit based guidance control, l-psi control, LQR formation control and L1 adaptive control for the control of multi agent system

 

More

SCIENTISTS WORKING ON PURSUIT BASED GUIDANCE CONTROL, L-PSI CONTROL, LQR FORMATION CONTROL AND L1 ADAPTIVE CONTROL FOR THE CONTROL OF MULTI AGENT SYSTEM

MODELING OF AIRFIELD AND AIRSPACE SCENARIO PERTAINING TO AN AIRPORT, SIMULATION OF AIRPORT WITH REALISTIC FLIGHT SCHEDULES

MODELING OF AIRFIELD AND AIRSPACE SCENARIO PERTAINING TO AN AIRPORT, SIMULATION OF AIRPORT WITH REALISTIC FLIGHT SCHEDULES

Modeling of airfield and airspace scenario pertaining to an airport, simulation of airport with realistic flight schedules

The airfield scenario was modeled based on the

More

SCIENTISTS WORKING ON MODELING OF AIRFIELD AND AIRSPACE SCENARIO PERTAINING TO AN AIRPORT, SIMULATION OF AIRPORT WITH REALISTIC FLIGHT SCHEDULES

NOVEL SCHEME FOR BASELINE FLIGHT CONTROLLER DESIGN

NOVEL SCHEME FOR BASELINE FLIGHT CONTROLLER DESIGN

Novel scheme for baseline Flight Controller Design

 The flight controller is developed using Nonlinear Dynamic Inversion (NDI) in combination with time scale separation,

More

SCIENTISTS WORKING ON NOVEL SCHEME FOR BASELINE FLIGHT CONTROLLER DESIGN

SIMILARITY BASED STABILITY AND CONTROL CLEARANCE FOR STORES INTEGRATED ON TO FRONTLINE FIGHTER AIRCRAFT OF INDIAN AIR FORCE

SIMILARITY BASED STABILITY AND CONTROL CLEARANCE FOR STORES INTEGRATED ON TO FRONTLINE FIGHTER AIRCRAFT OF INDIAN AIR FORCE

Similarity based stability and control clearance for stores integrated on to frontline fighter aircraft of Indian Air Force

 The objective is to ensure aeromechanical cle

More

SCIENTISTS WORKING ON SIMILARITY BASED STABILITY AND CONTROL CLEARANCE FOR STORES INTEGRATED ON TO FRONTLINE FIGHTER AIRCRAFT OF INDIAN AIR FORCE

ELECTRO-MECHANICAL ACTUATOR HEALTH MONITORING

ELECTRO-MECHANICAL ACTUATOR HEALTH MONITORING

Electro-Mechanical actuator health monitoring

Off late, aircraft uses a combination of pneumatic, hydraulic, and electric systems.

More

SCIENTISTS WORKING ON ELECTRO-MECHANICAL ACTUATOR HEALTH MONITORING

BEARING HEALTH CONDITION MONITORING

BEARING HEALTH CONDITION MONITORING

Bearing health condition monitoring

Condition monitoring is used to dynamically monitor various engine parameters and helps in detecting the faults before a catastrophic

More

SCIENTISTS WORKING ON BEARING HEALTH CONDITION MONITORING

GEO-FENCING AND TAGGING

GEO-FENCING AND TAGGING

Geo-fencing and tagging

Geo-location technique is developed in order to determine the location of the target geological coordinates from the image captured from the UAV o

More

SCIENTISTS WORKING ON GEO-FENCING AND TAGGING

IMAGE REGISTRATION AND FUSION

IMAGE REGISTRATION AND FUSION

Image registration and fusion

Image registration is pre-request for image fusion. There are many techniques are available in open literature.

More

SCIENTISTS WORKING ON IMAGE REGISTRATION AND FUSION

MULTI-SENSOR DATA FUSION TECHNIQUES FOR ENGINE HEALTH MONITORING

MULTI-SENSOR DATA FUSION TECHNIQUES FOR ENGINE HEALTH MONITORING

Multi-sensor data fusion techniques for Engine health monitoring

An aircraft engine is the component of the propulsion system for an aircraft that generates mechanical po

More

SCIENTISTS WORKING ON MULTI-SENSOR DATA FUSION TECHNIQUES FOR ENGINE HEALTH MONITORING

PHYSIOLOGICAL SIGNAL PROCESSING FOR PILOT WORKLOAD ASSESSMENT

PHYSIOLOGICAL SIGNAL PROCESSING FOR PILOT WORKLOAD ASSESSMENT

Physiological signal processing for pilot workload assessment

Aviation safety has been the primary focus in the industry.

More

SCIENTISTS WORKING ON PHYSIOLOGICAL SIGNAL PROCESSING FOR PILOT WORKLOAD ASSESSMENT

SENSE AND AVOID TECHNIQUES FOR UAS

SENSE AND AVOID TECHNIQUES FOR UAS

Sense and Avoid techniques for UAS

Unmanned Aerial Vehicle (UAV) has become a quiet a bit popular over the last 10 years because of its humongous growth in both military

More

SCIENTISTS WORKING ON SENSE AND AVOID TECHNIQUES FOR UAS

REAL TIME SENSOR FUSION ARCHITECTURE FOR UNMANNED AERIAL VEHICLES

REAL TIME SENSOR FUSION ARCHITECTURE FOR UNMANNED AERIAL VEHICLES

Real time sensor fusion architecture for Unmanned aerial vehicles

 

More

SCIENTISTS WORKING ON REAL TIME SENSOR FUSION ARCHITECTURE FOR UNMANNED AERIAL VEHICLES

OPTIMIZATION ALGORITHMS FOR MEMS IMU CALIBRATION

OPTIMIZATION ALGORITHMS FOR MEMS IMU CALIBRATION

Optimization algorithms for MEMS IMU calibration

Standard IEEE Calibration methodology and test procedure followed to calibrate MEMS IMU.

More

SCIENTISTS WORKING ON OPTIMIZATION ALGORITHMS FOR MEMS IMU CALIBRATION

EKF BASED ALGORITHM FOR STORE SEPARATION TRAJECTORY ESTIMATION OF LCA

EKF BASED ALGORITHM FOR STORE SEPARATION TRAJECTORY ESTIMATION OF LCA

EKF based algorithm for store separation trajectory estimation of LCA

Trajectory of a separated store from LCA has to be estimated with its standalone inertial measuremen

More

SCIENTISTS WORKING ON EKF BASED ALGORITHM FOR STORE SEPARATION TRAJECTORY ESTIMATION OF LCA

ENHANCED AND SYNTHETIC VISION SYSTEM

ENHANCED AND SYNTHETIC VISION SYSTEM

Enhanced and Synthetic Vision System

Development of Enhanced Synthetic Vision System (ESVS) for transport aircraft is one of the major activities initiated by Multi Senso

More

SCIENTISTS WORKING ON ENHANCED AND SYNTHETIC VISION SYSTEM

HUD SYMBOLOGY DEVELOPMENT FOR REGIONAL TRANSPORT AIRCRAFT

HUD SYMBOLOGY DEVELOPMENT FOR REGIONAL TRANSPORT AIRCRAFT

HUD Symbology development for regional transport aircraft

Working towards indigenous development of advance avionics technologies namely Enhanced Vision System (EVS), Syn

More

SCIENTISTS WORKING ON HUD SYMBOLOGY DEVELOPMENT FOR REGIONAL TRANSPORT AIRCRAFT

MULTI-SENSOR DATA FUSION AND FILTERING TECHNIQUES

MULTI-SENSOR DATA FUSION AND FILTERING TECHNIQUES

Multi-sensor data fusion and filtering techniques

Multi sensor data fusion group of FMCD has developed advanced multi sensor data fusion techniques and algorithms for pro

More

SCIENTISTS WORKING ON MULTI-SENSOR DATA FUSION AND FILTERING TECHNIQUES

Last updated on : 12-11-2020 05:13:58pm