Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates used for thr guidance based on time difference of arrival
This paper discusses the problem of determining a kinematics (in terms of transfer function, as far as possible) of parameters of the motion of an aircraft expressed in the curvilinear coordinate system and control accelerations expressed in a rectangular coordinate system. Examples of curvilinear c...
Saved in:
Main Authors: | V. V. Legkostup, V. E. Markevich |
---|---|
Format: | Article |
Language: | English |
Published: |
Belarusian National Technical University
2021-04-01
|
Series: | Системный анализ и прикладная информатика |
Subjects: | |
Online Access: | https://sapi.bntu.by/jour/article/view/498 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Methodology of determining of the transfer function of engagement kinematics of accelerations of an aircraft and its elliptic coordinates in alternative representation
by: V. V. Legkostup
Published: (2021-10-01) -
Method of Obtaining a Control Low Using a Synergetic Approach for the Problem of Aircraft Guidance Along a Hyperbola
by: V. V. Legkostup, et al.
Published: (2022-04-01) -
Method for determining of statistical characteristics of evaluated distance obtained from measurements of Doppler frequency offsets
by: V. V. Legkostup
Published: (2022-06-01) -
Procedure of the Synthesis of Control Device by the Method of Analytical Design of the Optimal Regulator for the Problem of Aircraft Guidance Along a Hyperbola
by: V. V. Legkostup, et al.
Published: (2022-03-01) -
Increase of the coordinate measurement accuracy in the multi-static radar in case of the receiving position placement on the aerial vehicle
by: V. V. Legkostup, et al.
Published: (2019-06-01)