Email this article Direct Method for Forming the Optimal Open Loop Control of Aerial Vehicles
- Authors: Korsun O.N.1,2, Stulovskii A.V.1,3
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Affiliations:
- State Research Institute of Aviation Systems
- Moscow Institute of Aviation (National Research University)
- Moscow Institute of Physics and Technology
- Issue: Vol 58, No 2 (2019)
- Pages: 229-243
- Section: Control Systems for Technological Processes
- URL: https://journal-vniispk.ru/1064-2307/article/view/220329
- DOI: https://doi.org/10.1134/S1064230719020114
- ID: 220329
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Abstract
A direct method for finding the optimal open loop control of an aircraft is proposed. It is based on the preliminary parameterization of controls with the subsequent parameter estimation using the numerical minimization of a given functional. Conditions for the application of this method and possible constraints are discussed. The efficiency of the method is confirmed by examples that use the results of simulation and flight data. The results are compared with the solutions obtained using the classical approach to finding the optimal control based on the solution of a two-point boundary value problem.
About the authors
O. N. Korsun
State Research Institute of Aviation Systems; Moscow Institute of Aviation (National Research University)
Author for correspondence.
Email: marmotto@rambler.ru
Russian Federation, Moscow, 125319; Moscow, 125993
A. V. Stulovskii
State Research Institute of Aviation Systems; Moscow Institute of Physics and Technology
Email: marmotto@rambler.ru
Russian Federation, Moscow, 125319; Dolgoprudnyi, Moscow oblast, 141700
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