Flight Control System Using Zigbee Wireless Sensors Engineering Essay

Flight Control System Using Zigbee piano tuner Sensors Engineering renderAbstract- This paper presents the future concept of escapism check out administrations that is named as Fly-By-Sensors (FBS) leak reign all over system. It can be utilise for correspondling and monitoring of an in- career functions, taking score and landing, voice communication etc. and can be employed on any kind of telephone line vehicle including Unmanned Air Vehicles, Quad rotor, airlike Vehicles, Drones, Jet air craft, commercial air craft etc. Nowadays, a fly-by-wire (FBW) flight control system of Air vehicles is employed for last few eld in aircrafts through which the internal and external functions of aircraft are controlled and monitored by electrical signals which are hereditary and received by electrical wires. The proposed idea is based on Zigbee Wireless Sensor entanglement that can be implemented on any air vehicle by utilize Zigbee Wireless Sensors that are piteously cost, low power, reliable and secure to control and monitor the internal and external functions of the air vehicles. The electrical signals, for controlling and monitoring of internal and external functions of air vehicle, in Fly-By-Sensors (FBS) flight control system will be deportted and received by using Zigbee wireless sensor engagement. The proposed idea will bring singular improvements in the field of avionics and aerospace.Keywords-component Zigbee Wireless Sensors FBS FBW flight control system of Air Vehicles.Introduction (Heading 1)The flight companies are in a struggle to reduce their air craft operational and chief(prenominal)tenance costs, saving fuel outlay and the gross take-off-weight of the air vehicles to carry as many as lend oneselfful things for civil and war machine purposes. In past several applications of Fly-By-Wire (FBW) flight control systems to civil aircrafts had been experienced. In FBW flight control systems the commands for controlling of the aircrafts i nternal and external functions are computed by the on board flight control computer on the basis of instructions by the buffer zone and without any mechanical linkage1. This resulted in the reduction of pilot workload and in general improvement of the Flying Qualities (FQ) characteristics. However the eminent development costs of a FBW flight control system made it unaffordable for the small aircrafts 2. Moreover, FBW flight control system is the ability to exhibit aircraft configurations and parameters which provide increased aerodynamic efficiency, but at a cost of reduced natural perceptual constancy. Moreover, this can grow instability of the aircraft at specific speeds and height conditions (or flight envelope).However, maintenance and troubleshooting of air vehicles, such as fault undercover work and monitoring systems of modern fly-by-wire (FBW) flight control system cannot detect faulty location accurately, so that experts can troubleshoot them in a shorter time. Howeve r, troubleshooting time depends mainly on the personnels skillfulness and experience 3.Flight Control SystemsFly-By-Optics(FBO) flight control systemFBO control system as the name implies that this kind of flight control system is based on the light signals which are transmitted through optical fibers. It uses electronic signals, transmitted through the fiber optics inside the air vehicles to control the employed electro-hydraulic actuators such as flaps, spoilers, slats, ailerons and rudder, in response to infix commands. Some times, it is used because of higher transfer data rates. The data generates by the software and interpret by the controller. It is also called as fly-by-light flight control systems.Power-By-Wire (PBW) flight control system 4Power-by-wire (PBW) is a control systems employed in some aircrafts to eliminate the bulky and heavy hydraulic circuits to replace by self contained electro-hydraulic actuators or electrical power circuits that are controlled by the digi tal flight control computers.Proposed Fly-By-Sensors (FBS) Flight Control SystemThe proposed flight control system is Fly-By-Sensors (FBS) flight control system to employ on any kind of air vehicle. As the name implies this type of control system will base on in style(p) Zigbee technology which is low cost, low power consumption and short distance wireless communication technology that is developed for wireless personal area network (WPAN) 5. By using this technology, the reduction in high cost in the manufacturing of electrical wires, gross take off weight of the air vehicles, fast detection of faulty equipment, landing and taking off of the air craft on auto pilot function of the aircraft, synthetic rubberty, guarantor and so on, can be achieved.Zigbee Wireless TechnologyZigBee is similar to IEEE 802.15.4 protocol, which is a one of the latest research in the field of communications in short distance wireless communication technology. Its main advantages are low-power, short-di stance, low-complexity, self organization, low-speed, low-cost, and so on. It is widely using as monitoring and controlling devices in many fields. It is suitable for low data-rate and low power consumption applications 6.Figure Difference of other wireless network standards with Zigbee Network standards (Source www.zigbee.org)Zigbee CharacteristicsThe IEEE 802.15.4 or Zigbee standard includes the features of low power consumption that is needed just for two major(ip) modes (Tx/Rx or Sleep), high density of nodes per network, low costs and simple installation of devices. Following are some more features for ZigbeeIt operates on radio bands of 2.4GHz in this high band is used in most of the jurisdictions of world wide, 868/915 MHz, this lower band in the areas of North America, Europe, Australia and New Zealand.High density of network nodes which is up to 65,000 network nodes.Low in cost, complexity power consumption as compared to competing technologies.Data rates ranges are 250Kb ps for 2.45GHz, 40 Kbps for 915MHz and 20Kbps for 868MHz band.Handshaking and 3 Frequencies bands with 27 channels.Extremely low duty-cycle (Star, cluster tree and mesh topologies can be used in Zigbee technology with the devices named as network coordinators, routers and end devices.Figure Zigbee Devices CharacteristicsZigbee Wireless Network used for landing of aircraftZigbee technology has been used for landing of the Unmanned Air Vehicle (UAV) and tested. The results showed that the recognition rate is over 90%, and the calculated error of position in landing of the UAV is less than 3m with 5000m distance and 0.2m with a measure of 500m distance. 7.Figure Landing of UAV through Zigbee Wireless Sensors Networks 7.As the Figure 3 shows the landing of UAV by using Zigbee sensors so we propose that Zigbee devices can also be used to control the aircrafts or UAVs for taking off purposes too so that the function of auto pilot can be used in an unfavorable climate conditions for safety and security purposes.Figure Proposed Future Concept of Taking off of the Aircraft through Zigbee SensorsProposed Fly-By-Sensors (FBS) over Fly-By-Wire (FBW) flight control SystemIn FBW flight control system, as the all electrical signals to Electro Hydraulic Actuators, Aileron, flap, rudder etc. are transmitted through wires. So the cost and weight of electrical wires limits the FBW control system to the commercial aircrafts only. Moreover, maintenance and troubleshooting of the faulty electrical wires consumes time and cost. The Safety and security of FBW flight control system is costly and non reliable for long term usage.Whereas, FBS flight control system will have the following advantages over FBW or PBWIt will be cheaper to use Zigbee technology than using electrical wires as it will costs almost 80% more than using the wireless sensors.The low power feature of Zigbee wireless sensors makes it to use for years without rechargeable batteries.The operating radio frequency is li cense free that is 2.4GHz with 16 channelsFBS control system will provide the safe monitoring system for controlling the aileron, rudder, electro hydraulic actuators etc.The Zigbee wireless sensor can also provide the Voice communication between pilot and co-pilot and the be staff for commercial aircrafts.The promising features of Zigbee technology will improve the reliability in the in-flight fault diagnostics and identification (FDI) as well as fault-tolerant control (FTC).By using Zigbee wireless sensors we will achieve the remarkable decrease in weight of the aircraft that will also help in more stability of the aircraft. At the result, there will be increase the number of passengers, goods or any material for transport purposes etc.Proposed Fly-By-Sensors (FBS) Flight Control Systems Block draw StructureFigure Block Diagram of proposed FBS flight Control SystemsAs Figure 5 shows the commands from the Pilot or from the Autopilot function of the aircraft will transmit by Zigbee Wireless Sensor Network through the on board computer on the aircraft. This technology will also be used for voice communication and other communications purposes in aircrafts.ConclusionThe proposed idea of Fly-By-Sensors (FBS) flight control system by using Zigbee Wireless Sensors will be mend than Fly-By-Wire (FBW) if it will be employed on the air vehicles. Specifically the decrease in weight, manufacturing cost, maintenance costs, troubleshooting time, power consumption, fuel consumption and increase in stability, reliability, safety, security etc. will bring the remarkable benefits to the aircraft industry.AcknowledgmentThe research work was supported and assisted by University College of Engineering Technology, The Islamia University of Bahawalpur.