What is the reason for choosing height error gain in such a way that the frequency of height loop is below the bandwidth of the pitch attitude loop?(a) Efficient flight(b) Better Range(c) Stable and damped response(d) Better climb rateI had been asked this question in a national level competition.My doubt is from Autopilots, Height Control and Heading Control in division Autopilots and Flight Management Systems of Avionics

What is the reason for choosing height error gain in such a way that t

1.	What is the reason for choosing height error gain in such a way that the frequency of height loop is below the bandwidth of the pitch attitude loop?(a) Efficient flight(b) Better Range(c) Stable and damped response(d) Better climb rateI had been asked this question in a national level competition.My doubt is from Autopilots, Height Control and Heading Control in division Autopilots and Flight Management Systems of Avionics
Answer» Correct choice is (c) Stable and damped response For explanation I WOULD say: The height error GAIN is chosen so that the frequencymax is well below the BANDWIDTH of pitch attitude loop to ensure a stable and well damped height loop response. If the frequency is high, it might lead to oscillations in the vertical AXIS.

Discussion

No Comment Found

Related InterviewSolutions

Which one of the following is not a factor for calculating speed breaches by the FMS?(a) Aircraft weight(b) CG position(c) Wind and temperature models(d) Position of the aircraftThe question was asked in an interview for job.My enquiry is from Flight Management Systems topic in chapter Autopilots and Flight Management Systems of Avionics
Navigational functions are no longer available if the INS shuts down in an FMS.(a) True(b) FalseI had been asked this question by my college professor while I was bunking the class.This is a very interesting question from Flight Management Systems in portion Autopilots and Flight Management Systems of Avionics
What is the interval for updating data in the navigation database?(a) 1 hour(b) 1 month(c) 24 hours(d) 28 daysThis question was addressed to me in an international level competition.I would like to ask this question from Flight Management Systems in section Autopilots and Flight Management Systems of Avionics
Which one of the following is not a navigation mode used by FMS for computing position of the aircraft?(a) Inertial (IRS) – GPS(b) Inertial (IRS) – DME/DME(c) Inertial (IRS) – VOR/DME(d) GPS onlyI got this question in an international level competition.Question is taken from Flight Management Systems topic in chapter Autopilots and Flight Management Systems of Avionics
What is the output for the following system?(a) Aircraft position(b) All the fight data(c) Gyro and accelerometer values(d) Warning signals for wrong navigationI had been asked this question in an interview for job.I'm obligated to ask this question of Flight Management Systems in portion Autopilots and Flight Management Systems of Avionics
What filter is used by the FMS to estimate the position of the aircraft from various sensors?(a) Kalman filter(b) Position error filter(c) GPS filter(d) Gyro and accelerometer filterThis question was addressed to me in a national level competition.My query is from Flight Management Systems in section Autopilots and Flight Management Systems of Avionics
The standby FMC performs calculations even when both the FMC are fully functional.(a) True(b) FalseI have been asked this question in an international level competition.My doubt is from Flight Management Systems in portion Autopilots and Flight Management Systems of Avionics
Both FMS 1 & 2 get information from only one FMC in the case of ______(a) Independent mode(b) Loss of one FMC(c) Single mode(d) Double modeThis question was addressed to me in final exam.The question is from Flight Management Systems in section Autopilots and Flight Management Systems of Avionics
What operating mode of the FMS does the figure show?(a) Double mode(b) Independent mode(c) Single mode(d) Redundancy modeThis question was posed to me in semester exam.This question is from Flight Management Systems topic in division Autopilots and Flight Management Systems of Avionics
What is the number of Flight Management Computers used in a typical commercial aircraft?(a) 2(b) 1(c) 4(d) 3I have been asked this question in examination.I'd like to ask this question from Flight Management Systems in section Autopilots and Flight Management Systems of Avionics

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment