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Related Concept Videos

Titration Calculations: Weak Acid - Strong Base03:55

Titration Calculations: Weak Acid - Strong Base

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Calculating pH for Titration Solutions: Weak Acid/Strong Base
For the titration of 25.00 mL of 0.100 M CH3CO2H with 0.100 M NaOH, the reaction can be represented as:
49.1K
Titration Calculations: Strong Acid - Strong Base02:28

Titration Calculations: Strong Acid - Strong Base

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Calculating pH for Titration Solutions: Strong Acid/Strong Base
A titration is carried out for 25.00 mL of 0.100 M HCl (strong acid) with 0.100 M of a strong base NaOH. The pH at different volumes of added base solution can be calculated as follows:
(a) Titrant volume = 0 mL. The solution pH is due to the acid ionization of HCl. Because this is a strong acid, the ionization is complete and the hydronium ion molarity is 0.100 M. The pH of the solution is then:
33.8K
Calculating pH Changes in a Buffer Solution02:45

Calculating pH Changes in a Buffer Solution

58.0K
A buffer can prevent a sudden drop or increase in the pH of a solution after the addition of a strong acid or base up to its buffering capacity; however, such addition of a strong acid or base does result in the slight pH change of the solution. The small pH change can be calculated by determining the resulting change in the concentration of buffer components, i.e., a weak acid and its conjugate base or vice versa. The concentrations obtained using these stoichiometric calculations can be used...
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Calculating Standard Free Energy Changes02:49

Calculating Standard Free Energy Changes

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The free energy change for a reaction that occurs under the standard conditions of 1 bar pressure and at 298 K is called the standard free energy change. Since free energy is a state function, its value depends only on the conditions of the initial and final states of the system. A convenient and common approach to the calculation of free energy changes for physical and chemical reactions is by use of widely available compilations of standard state thermodynamic data. One method involves the...
24.8K
Calculating the Equilibrium Constant02:46

Calculating the Equilibrium Constant

37.7K
The equilibrium constant for a reaction is calculated from the equilibrium concentrations (or pressures) of its reactants and products. If these concentrations are known, the calculation simply involves their substitution into the Kc expression.
For example, gaseous nitrogen dioxide forms dinitrogen tetroxide according to this equation:
37.7K
Numerical Calculations01:24

Numerical Calculations

1.2K
In engineering applications, the representation of the numerical value is critical. Presenting or reporting the answer is one of the essential parts of engineering practices. Numerical calculations are performed using handheld calculators or computers since numerically accurate answers are always preferred.
The solution to a problem is obtained using different methods. While manually solving algebraic symbols is one of the most common methods, the graphical method is often preferred. Computers...
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Measurement of Extracellular Ion Fluxes Using the Ion-selective Self-referencing Microelectrode Technique
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Accurate Measurement Calculation Method for Interferometric Radar Altimeter-Based Terrain Referenced Navigation.

Juhyun Oh1, Chang-Ky Sung2, Jungshin Lee3

  • 1Agency for Defense Development, Yuseong P.O.Box 35, Daejeon 34186, Korea. juhyunoh@add.re.kr.

Sensors (Basel, Switzerland)
|April 12, 2019
PubMed
Summary

A new Interferometric Radar Altimeter (IRA) formula improves Terrain Referenced Navigation (TRN) accuracy. It accounts for wind effects, providing more precise calculations of the closest point

Keywords:
flight testinterferometric radar altimeterterrain referenced navigation

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Area of Science:

  • Aerospace Engineering
  • Navigation Systems

Background:

  • Terrain Referenced Navigation (TRN) relies on accurate altimetry.
  • Conventional methods using Euler angles are insufficient in dynamic flight environments with wind.
  • Interferometric Radar Altimeters (IRA) offer enhanced distance and angle measurements.

Purpose of the Study:

  • To develop and validate a new formula for calculating the 3D relative position of the closest point for TRN using IRA data.
  • To address the limitations of existing formulas in real-world flight conditions influenced by wind.

Main Methods:

  • Development of a novel mathematical formula to compute the relative position of the closest point.
  • Utilization of Interferometric Radar Altimeter (IRA) data, including slant range (R) and cross-track angle (θ).
  • Verification of the proposed formula using real flight data and TRN simulations.

Main Results:

  • The proposed formula incorporates effective look angles, accounting for wind effects.
  • Flight tests demonstrated differences between the conventional and proposed methods due to wind.
  • TRN simulations confirmed the superior accuracy of the new formula in calculating closest point positions.

Conclusions:

  • The new formula provides a more accurate calculation of the closest point for TRN in the presence of wind.
  • This advancement enhances the performance and reliability of TRN systems.
  • The study highlights the importance of considering aerodynamic factors in navigation algorithms.