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    Modification of unscented kalman filter using a set of scaling parameters

    , Article IET Signal Processing ; Volume 12, Issue 4 , 2018 , Pages 471-480 ; 17519675 (ISSN) Zarei Jalalabadi, M ; Malaek, M. B ; Sharif University of Technology
    Institution of Engineering and Technology  2018
    Abstract
    This work, based on the standard unscented Kalman filter (UKF), proposes a modified UKF for highly non-linear stochastic systems, assuming that the associated probability distributions are normal. In the standard UKF with 2n + 1 sample points, the estimated mean and covariance match the true mean and covariance up to the third order, besides, there exists a scaling parameter that plays a crucial role in minimising the fourth-order errors. The proposed method consists of a computationally efficient formulation of the unscented transform that incorporates N - 1, N ≥ 2, constant parameters to scale 2n(N - 1) + 1 sample points such that the 2Nth order errors are minimised. The scaling parameters... 

    Semi-optimal co-ordinated manoeuvres for aircraft conflict resolution

    , Article Aeronautical Journal ; Volume 109, Issue 1097 , 2005 , Pages 313-323 ; 00019240 (ISSN) Parastari, J ; Malaek, M. B ; Sharif University of Technology
    Royal Aeronautical Society  2005
    Abstract
    In this manuscript, a new concept of 2D-semi-optimal-circular-3-arced-path manoeuvres with constant speed for multiple aircraft cooperative conflict resolution is presented. This type of manoeuvres is based on appropriate commands to heading, speed and manoeuvreing time. According to aircraft turning dynamics, each aircraft manoeuvre is composed of three tangent circular arcs. The optimality of manoeuvres is based on the minimisation of weighted sum of kinetic energy for aircraft two-legged manoeuvres. In comparison, aircraft with lower weight factors bear more responsibility to resolve the conflicts. The effectiveness of the proposed algorithm for real time conflict resolution is... 

    Pre-mission activities for the space higher education

    , Article 61st International Astronautical Congress 2010, IAC 2010, 27 September 2010 through 1 October 2010, Prague ; Volume 3 , 2010 , Pages 2360-2366 ; 9781617823688 (ISBN) Vernoosfaderani, M. T ; Malaek, M. B ; Jazebizadeh, H ; Sharif University of Technology
    2010
    Abstract
    Based on general "System Theory", a system when it comes to its intended operational life; must exhibits three distinguished phases of (1) Pre-mission, (2) Mission, and (3) Post-mission. During Pre-mission one evaluates the system elements readiness to conduct the mission; their proper configurations in addition to their support roles to conduct their organizational role. During Post-mission, we check whether our evaluations were in fact, correct to the levels expected. Both pre and post mission phases are necessary for a successful mission. An education system; especially designed for space applications which aims to deliver the necessary workforce for the relevant industries and other... 

    A generic method for remote sensing satellites conceptual design and rapid sizing based on »design for performance» strategy

    , Article IEEE Aerospace and Electronic Systems Magazine ; Volume 33, Issue 2 , 2018 , Pages 34-51 ; 08858985 (ISSN) Ahmadi, A ; Kosari, A ; Malaek, M. B ; Sharif University of Technology
    Institute of Electrical and Electronics Engineers Inc  2018
    Abstract
    Some fundamental and unique characteristics of space are (1) global perspective, (2) above the atmosphere, (3) gravity-free environment, (4) abundant resources, and (5) exploration of space itself. If the mission doesn't rely on some fundamental and unique characteristics of space, it will likely cost more to do in space than in air or on Earth [1]. On the other hand, design of complex systems like satellites involves selecting design parameters (DPs) to satisfy the required constraints while meeting desired performance objectives. These parameters are often coupled, and their relationships not easily understood, and it makes the design an iterative process with high complexity [2]. But in... 

    Aircraft design cycle time reduction using artificial intelligence

    , Article Aerospace Science and Technology ; Volume 26, Issue 1 , 2013 , Pages 244-258 ; 12709638 (ISSN) Azizi Oroumieh, M. A ; Malaek, M. B. S ; Ashrafizaadeh, M ; Taheri, M. S ; Sharif University of Technology
    2013
    Abstract
    In this work we show how Artificial Intelligence (AI) could effectively be used to expedite the decision making process in the early stages of the aircraft design process. We employ both Fuzzy Logic (FL) and Neural Network (NN) as two different schemes of the AI. The developed tools are intended to help to select the proper combination of engine thrust, wing area and the aircraft weight without going through elaborate details of other direct approaches. We further show how the AI could be applied to the specific class of light business jets which serves to validate these schemes. The results indicate the effectiveness of the AI approach in the preliminary aircraft design process. The actual...