Useful links

##
1. Introduction

First stage of math education contains familiarization with numbers. Then unknown "*x*" was introduced. I thought: "Why do you need "*x*"? Does not application of numbers quite enough?" A lot of my friends had similar opinion. One my colleague told me similar story. Then he noticed that I have used notation *f* for real function of real argument. He said: "Your notation is not correct. You should use *f*(*x*) notation". I explained that *f* means actual function but *f*(*x*) is value of function where argument is equal to *x* (*f*(*x*) is also named potential function).
Indeed usage of *f* is next step of abstraction. A lot of
people tell:"I do not
theoretician I am practitioner" A lot of people told me that they are
practitioners. But "practitioner" term as itself does not have meaning. So I asked people: "Who is practitioner?"
My public opinion poll yield following well known list of answers:

- I am an engineer, so I do not need object oriented paradigm. (This engineer had used ALGOL at 1995, he used a lot of labels instead "begin ... end" construction.
- I do not have no time for theoretical study.
- I prefer simplicity. (This man is not familiar with code reuse).
- High quality contradicts rapid development.

Any good IT specialist can himself/herself extend this list of antipatterns. My own opinion is: "Theory is useful for practice". So I placed "?" at this article title. All my articles contain a lot of theory. Main accent of this article is usefulness of theory. Following story proves that application of theory is time saving.

I was often condemned by my colleagues: “You are reading irrelevant books” One my colleague many years tried to find analytical solution of on engineering ordinary differential equation. I told him that existence of such solution is extraordinary event. I read the book I. Kaplansky, “Differential Algebra”, Hermann (1957). Roughly speaking this book explains the fact that existence of analytical solution is extraordinary event.
The colleague answered me that the book is irrelevant. “We are not mathematicians but we are engineers” He did not find analytical solution. I am not sure that this solution would be useful because numerical solution
takes part of one second.
A lot of colleagues told me that they are very busy. So they do not read smart books. They told that I have a lot of time and so I read a lot of books.
However I do not spend time for useless tasks.
Maybe reading of smart books provides time-saving?

##
2. Background.

Rigorous math has laconism, definiteness and context dependence. Meaning of below notation

is presented in following table

N | Element | Type |

1 | *f*, *g* | Real function of real argument |

2 | *a* | Real number |

3 | *v* | Real vector which dimension is equal to *n* |

My friend thought that "*x*" in "*f*(*x*)" is always real number. However "*x*" can be also a vector or a function. Following table represents different types of "*x*"

is presented in following table:

N | Type of argument | Expression | Meaning | Type of result |

1 | Real number | *f*(*a*) | Result of calculation of *f* if argument is equal to *a* | Real number |

2 | Real function of real argument | *f*(*g*) | Composition of functions *f* and *g* | Real function of real argument |

1 | Real vector which dimension is equal to *n*
| *f*(*v*) | Componentwise calculation of
*f* | Real vector which dimension is equal to *n* |

Samples of applications of this theory is presented below.

## 3. Functions

### 3.1 Base interface

Talk about *f* and *f*(*x*) was happened at 1977. A lot of engineers thought that FORTRAN is the best language and at that time usefulness of theory was not evident for software development. Only object oriented paradigm provide good abstract expression of function. Following interface represents base interface for all one variable function:

public interface IOneVariableFunction : IObjectOperation
{
object VariableType
{
get;
}
}
public interface IObjectOperation
{
object[] InputTypes
{
get;
}
object this[object[] arguments]
{
get;
}
object ReturnType
{
get;
}
}

Above interface is specification of `IObjectOperation`

interface. The `IObjectOperation`

very general interface which calculates object by set of arguments. The `IOneVariableFunction`

is not always real function of real argument. The `ReturnType`

and `VariableType`

properties are types of function return and argument respectively.

### 3.2 Examples

#### 3.2.1 Explicit formula

A set functions can be represented by explicit formula. Samples of explicit expressions are presented below:

These expressions represent the same function. However arguments of the functions are different. Moreover types of arguments

*p* and

*t* can be different.

#### 3.2.2 Table

A lot of functions used in science and engineering are defined by experiment. These functions are tabulated. Example of tabulated function is presented below:

Following picture represents sample of application of tabulated function:

The **Chart** element is a table. Columns of this table are *X* (abscissa) and *Y* (ordinate). It have following outputs:

N | Parameter | Symbol | Type |

1 | Array of *X* values | X | `double[dimension]` |

2 | Array of *Y* values | Y | `double[dimension]` |

3 | Minimal element among *X* values | X_1 | `double` |

4 | Minimal element among *Y* values | Y_1 | `double` |

5 | Maximal element among *X* values | X_2 | `double` |

6 | Maximal element among *Y* values | Y_2 | `double` |

7 | Function *f* defined by table | Function | `double f(double)` |

Following picture represents user interface of these parameters:

Follownig picture presents demo application of tabulated functions:

Properties of objects **F**, **G** and **H** are presented below

The **F** has single formula (*Formula 1*). The formula has single variable *f*. Otherwise the *f* variable is linked to `Double f(Double)`

*Function* of **Graph** object. The **G** object has three variables and two output formulae.

N | Variable name | Type | Comment |

1 | *f* | `Double f(Double)` | *Formula_1* of **F** |

2 | *g* | `Double f(Double)` | Function from **Chart** |

3 | *t* | `Double` | Time variable |

N | Formula | Type | Comment |

1 | *Formula_1* | `Double` | Real value of function which depends on time variable |

2 | *Formula_2* | `Double f(Double)` | Composition of functions *f* and *g* |

And at last **H** object has following variables and output formulae

<><>< />

N | Variable name | Type | Comment |

1 | x | `Double` | *Formula_1* of **
G** = Value of **Chart** function where argument equals to time |

2 | *f* | `Double f(Double)` | *Formula_2* of **
G** = Composition of **Chart** function and *Formula_1* from **F** = Composition of **Chart** function with ifsels |

3 | *t* | `Double` | Time variable |

N | Formula | Type | Comment |

1 | *Formula_1* | `Double` | Value of *x* = Value of **Chart** function where argument equals to time |

2 | *Formula_2* | `Double` | *f*(*t*) value, where *f* is composition of **Chart function** with itself, *t* is time |

Following picture represents *Formula_1* and *Formula_1* of **G**.

Red and Blue curve are charts of **Chart** function and composition of **Chart** function with itself respectively. Note that this software assumes that X limits of table value of function equals to zero.

#### 3.2.3 Numerical calculation

There are a lot of math functions which do not have explicit expression. A lot of differential equations do not have explicit solutions. For example second order linear differential equation *y''*+*xy* = 0 (*x* is argument, '' means second total derivative) does not have explicit solution. The I. Kaplansky, “Differential Algebra”, Hermann (1957) book
contains prove of above fact. However numerical calculation yield these functions. Here numerical solution of *y''*+*xy* = 0 is considered. This differential equation is equivalent to following system of first order differential equations:

*y' = z*;

*z' = -xy*.

where *z = y'*. We consider following modification of above system:

Greek delta means Dirac delta function, *k* and *a* are real constants. This modified system also does not have explicit solution but presence of delta function makes equations more interesting. Following picture represents solution of above system.

The **Differential equation** object has following properties:

Where variable *a* is *Formula_1* of **Input** which is represented below

.

Following chart represents solution of differential equation system:

Red and blue curve represents *y* and *z* respectively. Jump of *z* is caused by presence of Dirac delta function as well as jump of *y* derivative. So numerical solution yield necessary function. However this function is rather *f*(*x*) than *f*. It is potential function, i.e. calculation for concrete value of argument. But a lot of tasks require actual *f*, i.e. function as global. For example composition of functions requires function as global. Application of following **Accumulator** component yield actual (global) *f*.

This component has following variables:

The **Accumulator** is very similar to Transport Delay of Simulink. **Accumulator** transfers potenial functions *y*(*t*), *z*(*t*) of **Differential equation** to actual ones, i.e. *y* and *z* respectively. These actual functions are numerically calculated on [0,1] interval. Step of calculation is equal to 0.01, number of steps is equal to 100. These actual functions can be composed. The **Composition** yield this composition. Properties of this component are presented below:

Variables of **Composition** are presented below

N | Variable name | Type | Comment |

1 | *f* | `Double f(Double)` | *Differential_equation_y* of **
Accumulator** = *y* of **Differential equation** as actual function |

2 | *g* | `Double f(Double)` | *
Differential_equation_z* of **
Accumulator** = *z* of **Differential equation** as actual function |

Output of **Composition** is function composition *f*(*g*) or *y*(*x*) because *f* and *g* of **Composition** are respectively actual *y* and *z* of **Differential equation**. Composition result is presented below:

## 4. Practical Applications

Above samples are rather artificial then practical. Here I would like to prove usefulness of theory for practice.

### 4.1 Parametric Identification of Transfer Functions
in the Frequency Domain

Here is a survey of Parametric Identification of Transfer Functions
in the Frequency Domain. We would like identify parameters of following third order transfer function:

Assume that frequency response is defined by experiment. Following picture represents idea of identification is presented at following pictures.

We would like yield such values of constants *k*, *T*_{1}, *T*_{2}, *T*_{3} that theoretical dependence of frequency response approximate experimental values. Experimental values are red crosses of above charts. Blue curves theoretically calculated frequency responses. Identification yield good approximation of experimental data. Theoretical dependencies of frequency response and phase response of above transfer function are presented below:

tan^{-1} and phase response are expressed in degrees. So we would like approximate experimental data by above formula of frequency response. Following picture contains solution of this task

The **Graph** element contains following table of frequency response which yield experiment.

*X* and *Y* columns of this table correspond to frequency and frequency responce. The **Formula** component contains following regression formula:

Above formula is explicit expression of frequency response. Argument *p* of this formula is a vector (array) of **Graph** *X* coordinates. So argument of function is not real number but real vector. Constants of above formula correspond to parameters of transfer function by following way:

N | Constant of formula | Parameter of transfer function |

1 | *k* | *k* |

2 | *a* | *T*_{1} |

3 | *b* | *T*_{2} |

4 | *c* | *T*_{3} |

So above formula represents theoretical frequency response. The **Processor** component yield such values of *k*, *T*_{1}, *T*_{2}, *T*_{1} (or *k*, *a*, *b*, *c* of **Formula**) that experimentally defined values of frequency response are approximated by theoretically calculated values. Properties of **Processor** component are presented below:

Number 0 correspond to both *Formula_1* of **Formula** and *Y* of **Graph**. It means that experimentally defined values of frequency response is approximated by theoretical ones. All marked by -1 expressions are not taken into account in regression process. However ** Formula** component has other formulae:

First formula is frequency response. But argument of this formula is time variable *t*. Second one is phase response. Application of these formulae is indication of frequency response:

Theoretical function *f* of frequency response is used twice. First of all it is used as *f*(*p*) where *is* vector. Also it is used as *f*(*t*) where *t* is (nonconstant) real number. Application of 2 formulae for single function is not a good idea. Following picture represents application of single function.

The **Formula** object calculates *f*(*t*), where *t* is time variable. Then **Accumulator** makes actual *f* from *f*(*t*). And at last **F(X)** object calculates application of this function to *X -* coordinates of **Graph** object.
Properties of **F(X)** are presented below

### 4.2 Artificial Earth satellite

Here following tasks are considered

- Determination of motion parameters;
- Generation of text document;
- Visualization;
- Audio support.

All these tasks use motion parameters as time functions in different context. Orbit determination uses vector values, visualization uses functions of time variable. However single set of parameters are being used for all this tasks. Roughly speaking actual *f* instead potential *f*(*x*) is used.

#### 4.2.1 Motion model

Motion model of spacecraft is already described here. But I have copied text for easy reading.

The motion model of an artificial satellite is a system of ordinary differential
equations that describe the motion in a Greenwich reference frame:

where
are the coordinates and components of velocity respectively,
is angular velocity of Earth, and
are components of the summary external acceleration. The
current model contains gravitational force and the aerodynamic one. These
accelerations can be defined by the following formulae:

The following table contains meaning of these parameters:

Component of ordinary differential equations is used for above equations. This
component does not have a rich system of symbols and uses lower case variables
only. However this component supports rich system of comments which is presented
below:

These comments can contain mappings between variables and physical parameters.
Independent variables of equations (*x*, *y*, *z*, *u*,
*v*, *w*) are checked in right part. Mapping between these
variables and

The component represents differential equations in the following way:

Besides independent variables equations contain additional parameters. The
following table contains mapping of these parameters:

Some of these parameters are constants. Other parameters should be exported.
Constants are checked and exported parameters are not checked below:

Exported parameters concern with gravity and atmosphere models. These models are
contained in external libraries. The following picture contains components of
motion model.

The **Motion equations** component is considered above component of
ordinary differential equations. These equations have feedback. Right parts of
equations depend on gravitational forces. Otherwise gravitational forces depend
on coordinates of the satellite. The **Vector** component is used
as feedback of **Motion equations**.

This picture has the following meaning. Variables *x*, *y*, *z*,
*u*, *v*, *w* of **Vector** component are
assigned to *x*, *y*, *z*, *u*, *v*, *w*
variables of **Motion equations**. Input and output parameters of
**Vector** are presented below:

Components **Gravity**, **Atmosphere** are objects
obtained from external libraries which calculate Gravity of Earth and Earth's
atmosphere respectively. Both these objects implement `IObjectTransformer`

interface. The **G-transformation** and **A-transformation**
objects are helper objects which are used for application of **Gravity**,
**Atmosphere** objects respectively. Properties of **
G-transformation** are presented below:

The above picture has the following meaning. The **G-transformation**
is connected to **Gravity** object. This object corresponds to
exported `Gravity`

class (code of `Gravity`

class is above
this text). The `Gravity`

class implements `IObjectTransformer`

interface. Input parameters of `Gravity`

are coordinates which are
labeled by "*x*", "*y*", "*z*" labels. So above comboboxes
are labeled by *x*", "*y*", "*z* labels. The above picture
means that parameters *x*", "*y*", "*z*" are assigned to
*Formula_1*, *Formula_2*, *Formula_3* of **Vector**
component. Otherwise *Formula_1*, *Formula_2*, *Formula_3*
of **Vector** are assigned to *x*, *y*, *z* of
**Motion equations**. However **Motion equations**
component uses parameters of **G-transformation**:

This picture means that parameters *a*, *b*, *c* of *a*,
of **Motion equations** are assigned to parameters *Gx*, *
Gy*, *Gz* of **G-transformation**. So of Earth's

Gravity

function is exported to

**G-transformation**. The
Earth's atmosphere is exported in a similar way.

#### 4.2.2 Orbit determination

The following picture illustrates the problem of determination of the orbit.

We have an artificial Earth's satellite. There are a set of ground stations
which perform measurements. So we have measurements of distance and relative
velocity between stations and the satellite. Processing of these measurements
provides determination of orbit.

##### 4.2.2.1 Input Data

Input data contains measurements of distances and relative velocities. Special
components are used for this purpose. These components are presented below:

Ordinates of **Distance** component are measured distances and
ordinates of **Velocity** one are measured relative velocities.
Abscises of these components are indifferent. Other input data are represented
below:

The full list of input parameters is represented in the following table:

| Component name | Comment |

1 | Distance | Array of distance measurements |

2 | Velocity | Array of velocity measurements |

3 | Distance Time | Array of times of distance measurements |

4 | Velocity Time | Array of times of velocity measurements |

5 | Distance X | Array of *X* - coordinates of ground station which correspond to distance
measurements |

6 | Distance Y | Array of *Y* - coordinates of ground station which correspond to distance
measurements |

7 | Distance Z | Array of *Z* - coordinates of ground station which correspond to distance
measurements |

8 | Velocity X | Array of *X* - coordinates of ground station which correspond to velocity
measurements |

9 | Velocity Y | Array of *Y* - coordinates of ground station which correspond to velocity
measurements |

10 | Velocity Z | Array of *Z* - coordinates of ground station which correspond to velocity
measurements |

11 | Distance Sigma | Array of standard deviations of distance measurements |

12 | Velocity Sigma | Array of standard deviations of velocity measurements |

Let us comment on this table. We have two arrays of measurements. First array
*d*_{1}, *d*_{2}, ... contains measurements of
distance. Second one *V*_{1}, *V*_{2} ... contains
measurements of velocity. First two rows of the above table correspond to these
two arrays. Measurements *d*_{1}, *d*_{2}, ... are
performed in different times. Third row of above table corresponds to array of
times of these measurements. Similarly 4 - th row corresponds to array of times
of *V*_{1}, *V*_{2} ... measurements. A set of
ground stations is used for measurements. Suppose that *d*_{i} is
obtained by ground station which has coordinates *X*_{i}, *Y*_{i},
*Z*_{i}. The 5, 6, 7 th rows of table correspond to *X*_{i},
*Y*_{i}, *Z*_{i} arrays. Similarly 8 - 10 rows
correspond to coordinates of ground stations and *V*_{i}
measurements. Note that the different measurements have no equal accuracy. The
General linear method requires to use different weights for such measurements. A
new component
was developed for this purpose. It enables us to create
weighted selections. In case of orbit determination, measurements have different
variances. So we have
weighted least squares situation. So variances of measurements are needed.
Rows 11 and 12 contain arrays variances of *d*_{i} and *V*_{i}
respectively. Components **Distance Selection** and **
Velocity Selection** are "weighted selections" which contain measurements
and their variances. Properties of **Distance Selection** are
presented below:

This picture has the following meaning:

- Array of measurements is contained in ordinates of
**Distance**
component. - Array of variances is contained in ordinates of
**Distance Sigma**
component.

The **Velocity Selection** component is constructed in a similar
way. I've used the graph
component for the storage of the selection. It has been done
since the user would be able to try this example without a database. Really,
this scenario should use the connection to the database graph
.

##### 4.2.2.2 Nonlinear Regression

**Nonlinear regression** in
statistics is the problem of fitting a model.

to multidimensional *x*,*y* data, where *f* is a
nonlinear function of *x*, with regression
parameter θ.

Nonlinear regression operates with selections. This software implements two
methods of manipulation with selections. The first method loads selection
iteratively, i.e., step by step. The second one loads selection at once.

The architecture of nonlinear regression software that uses iterative regression
is presented in the following scheme:

Let us describe the components of this scheme. The iterator provides data-in
selections *x* and *y*. The *y* is the **Left part**
of fitting the equations. The **Transformation** corresponds to the
nonlinear function *f*, and generates the **Left part** of
the fitting model. The **Processor** coordinates all the actions
and corrects the **Regression parameters**.

The architecture of the software with loading selection at once is presented in
the following scheme:

The processor compares **Calculated parameters** with **
Selection**, calculates residuals, and then corrects **Regression
parameters**. In these two schemas, the **Iterator**,
**Selection**, and others are not concrete components. They are
components that implement interfaces of **Iterator**, **
Selection** etc. For example, a **Camera** component may
implement the **Selection** interface. Here, I'll consider examples
in brief. A more profound description is available in the
documentation of this project. Second scheme is used for determination of
orbits.

##### 4.2.2.3 Ingredients

The above picture contains general ingredients of nonlinear regression. Let us
consider ingredients related to orbit determination of orbits. The **
Selection** is already considered in 6.1. **Regression parameters**
are initial values of coordinates and components of velocity of the satellite.
These parameters are contained in **Motion equations** component.
These parameters are presented in the following picture:

As it is already noted, parameters *x*, *y*, *x*, *u*,
*v*, *w* are coordinates and components of velocity. Top part of
above picture contains values of these parameters before orbit determination.
Bottom one contains values after orbit determination. These parameters are being
changed during orbit determination. Transformation stage contains the following
steps:

- Calculation of trajectory of satellite
- Calculation of time shifts
- Calculation of distances and velocities

The **Accumulator** component performs calculation of trajectory
parameters as actual functions. Let us explain what is the actual function.
There are two points of definitions of function. According to potential point
function *f*(*t*) is calculation of *f* by known argument
*t*. Actual point means that function *f* is single (actual)
object. Actual function can be obtained from potential by calculation of values
of *f*(*t*) at different values of *t*. The **Motion
equations** component performs potential calculation of motion parameters
and **Accumulator** object transforms these potential functions to
actual ones. Properties of **Accumulator** are presented below:

According to these properties, **Accumulator** calculates *f*(*t*_{0}),
*f*(*t*_{1}), *f*(*t*_{2}), ...
where *t*_{0} = 1770457504 (Start), *t*_{i+1}
- *t*_{i} = 10 (Step). Number of values of argument is
equal to 2500 (Step count). So **Accumulator** stores *f*(*t*_{0}),
*f*(*t*_{1}), *f*(*t*_{2}) and for
any *t*_{0} < *t* < *t*_{2500}. Then *f*(*t*)
is obtained by interpolation by polynom of third degree. It should be noted that
measurements of distances and velocities are not instant since
speed of
light is finite. Ground station sends signal at *t*_{1} time,
then satellite sends reflected signal at *t*_{2} time and then
ground station receives signal at *t*_{3} time. The time of
measurement is *t*_{3}. However measurement of distance is not
distance between satellite and station at *t*_{3}. It is equal (*d*_{1}
- *d*_{2}) / 2 where *d*_{1} is distance between
station at *t*_{1} time and satellite at *t*_{2}
time and similarly *d*_{2} is distance between station at *t*_{3}
time and satellite at *t*_{2} time. The **Difference**
and **Time + Shift** components enable us take into account this
circumstance. Properties of **Difference** component are presented
in the following picture:

Output of this component is used by **Time + Shift**. Properties of
**Time + Shift** are presented below:

This component calculates arrays of times of reflection of signals by the
satellites. Component **Delta** is helper. It has the following
properties:

The **Measurements** component calculates measurements of distance
and velocity. This component has the following properties:

This parameters are compared with selections. The **Processor**
component performs such computation or (using another term) regression.
Regression formula is presented below:

**Processor** component reflects this formula. Properties of this
component are presented below:

Left part of above window corresponds to *x* of regression formula. In
considered case components of *x* are coordinates and components of
velocity. The following table contains components of vector *x*.

| Physical parameter | Identifier |

1 | *X* | *Motion Equations/Motion Equations.x* |

2 | *Y* | *Motion Equations/Motion Equations.y* |

3 | *Z* | *Motion Equations/Motion Equations.z* |

4 | *V*_{x} | *Motion Equations/Motion Equations.u* |

5 | *V*_{y} | *Motion Equations/Motion Equations.v* |

6 | *V*_{z} | *Motion Equations/Motion Equations.w* |

Middle part of above window contains *f*(*x*) of regression
formula. The *f*(*x*) vector contains two subvectors *Formula_1*
and *Formula_2* which belong to **Measurements** components.
These subvectors are calculated values of distances and velocities. Right part
of above window corresponds to *y* of regression formula. Vector *y*
contains two selections which correspond to distance and velocity measurements
respectively. Click to *Iterate* button initiate step of nonlinear
regression.

##### 4.2.2.4 Resume

Orbit determination requires motion parameters as actual functions. Moreover shifted by time delay functions are required. However motion equations do not have explicit solution. So **Accumulator** component is used. Roughly speaking it transforms potential *f*(*x*) function to actual *f* one.

#### 4.2.3 Orbit determination container

Above tasts are already described in my article. Here extended task is described. Orbit determination task is aggregated for more easy further development. Aggregation result is presented below:

Extended task is presented at following picture:

It contains also video, audio and document generation.

#### 4.2.4 Video

Video task is rather "*f*(*t*)" than "*f*" where *t* is time variable. Following components are meant for video support:

The **Camera** component is virtual WPF Perspective Camera. It has following properties:

The **Globe** is 3D model of Globe. It contains XAML 3D model and texture. **Globe** and **Camera** are virtually installed on **Base frame** and **Camera Frame** respectively. Both **Base frame** and **Camera Frame** are virtual 3D
Cartesian coordinate system These systems are meant for motion simulation of **Camera** with respect to **Globe**. **Base frame** is Greenwich reference frame. Other frames are constructed by following way:

This picture has following meaning. Motion of **Frame 1**, **Frame 2**, **Camera Frame** regarded as relative motion with respect to **Base frame**, **Frame 1**, **Frame 2**. Let *x*, *y*, *z* be coordinates of the satellite than
**Frame 1** has nonzero linear shift (*x*, *y*,*z*) with respect to **Base frame**. Also this frame is rotated by longitude around *Z* axis. **Frame 2** is not shifted with respect to **Frame 1**. However it is rotated by latitude angle around *Y* - axis. **Camera Frame**
has zero shift and following transformation matrix with respect to **Frame 2**

Visual image of these frames is presented below:

Where are latitude and longitude of the satellite respectively.
Axes of **Frame 1** are parallel to axes of *X'Y'Z'*, both frames are red at above picture. However center of **
Frame 1** coincides with center of mass of the satellite.
Axes of **Frame 2** are parallel to axes of *X''Y''Z''*, both frames are
blue at above picture and of **Frame 2** also coincides with center of mass of the satellite. Components **Angles** and **Quaternions** are meant for orientation calculations. Properties of **Angles** are presented below:

Variables *x*, *y*, *z* are just coordinates *x*, *y*, *z* of the satellite. *Formula_1*, *Formula_2* are exactly longitude and latitude of the satellite respectively. Rotation of **Frame 1** and **Frame 1** can be expressed by following quaternions respectively:

**Quaternions** component calculates necessary data for above quaternions. Properties of **Quaternions** component are presented below:

Following pictures and tables represent properties of **Frame 1** and *Frame 2*

.

Properties of **Frame 1**

N | Parameter name | Frame parameter | Imported parameter | Comment |

1 | *X* | *X* - relative shift of frame | *Orbit determination/Motion equations/Motion equations.x* | *X* coordinate of the satellite |

2 | *Y* | *Y* - relative shift of frame | *Orbit determination/Motion equations/Motion equations.y* | *Y* coordinate of the satellite |

3 | *Z* | *Z* - relative shift of frame | *Orbit determination/Motion equations/Motion equations.z* | *Z* coordinate of the satellite |

4 | *Q*0 | Real component of quaternion | *Quaternions.Formula_1* | cos(*longitude*/2) |

5 | *Q*1 | **i** - component of quaternion | *Quaternions.Formula_5* | 0 |

6 | *Q*2 | **j** - component of quaternion | *Quaternions.Formula_5* | 0 |

7 | *Q*3 | **k** - component of quaternion | *Quaternions.Formula_2* | sin(*longitude*/2) |

Properties of **Frame 2**

N | Parameter name | Frame parameter | Imported parameter | Comment |

1 | *X* | *X* - relative shift of frame | *Quaternions.Formula_5* | 0 |

2 | *Y* | *Y* - relative shift of frame | *Quaternions.Formula_5* | 0 |

3 | *Z* | *Z* - relative shift of frame | *Quaternions.Formula_5* | 0 |

4 | *Q*0 | Real component of quaternion | *Quaternions.Formula_1* | cos(*latitude*/2) |

5 | *Q*1 | **i** - component of quaternion | *Quaternions.Formula_5* | 0 |

6 | *Q*2 | **j** - component of quaternion | *Quaternions.Formula_5* | sin(*latitude*/2) |

7 | *Q*3 | **k** - component of quaternion | *Quaternions.Formula_2* | 0 |

**Camera frame** is meant for **Camera** optical axis orientation in the direction to center of Globe.

#### 4.2.5 Audio

Let us consider following audio support which blows sounds when satellite intersects Equator.

Following sounds are included in audio support:

- Blowing of "Up" word if satellite is moved from South hemisphere to North one;
- Blowing of "Down" word if satellite is moved from North hemisphere to South one.

This task is also rather "*f*(*t*)" than "*f*" where *t* is time variable.
Following picture represents components of this sample

The **Sound Recursive** is element which performs following reqursive calclulations:

*y*_{n}=*z*_{n};

*x*_{n}=*y*_{n-1};

where *z*_{n} is *z* - coordinate of satellite at *n*^{th} step of calculation. Since *z* > 0 at North hemisphere and *z*
< 0 at South we have following condition of Equator intersection.

N | Condition | Meaning |

1 | *z*_{n-1} < 0) AND (*z*_{n} > 0) | The satellite has intersected Equator from South hemisphere to North one |

2 | *z*_{n-1} > 0) AND (*z*_{n} < 0) | The satellite has intersected Equator from North hemisphere to South one |

The **Sound formula** component yields formulae of these conditions:

**Sound** component is meant for sound blowing according following table:

N | Condition parameter | Meaning | Sound file |

1 | Sound formula.Formula_1 = true | Satellite intersects equator plane from South to North | up.wav |

2 | Sound formula.Formula_2 = true | Satellite intersects equator plane from North to South | down.wav |

#### 4.2.6 Generation of document

In this sample actual function *f* is used. However this function has another argument. This argument is *Z-* coordinate of the satellite.

Besides calculation, any software needs generation of documents. Facilities
generation of documents are exhibited on forecast problem. Forecast document
contains parameters of satellite motion in times of equator intersections. The
following picture explains the forecast problem:

Satellite moves along its orbit. Parameters of motion correspond to the time
when it moves from South to North and intersects equator. Satellite intersects
equator when its *Z* - coordinate is equal to 0. If we have coordinates
and time as function of *Z*, then we can see necessary parameters are
values of these functions where *Z* = 0. The following picture represents
a solution of this task.

The **Delay** component has `FunctionAccumulator`

type.
This type is very similar to
Transport delay of Simulink. However

FunctionAccumulator

is more advanced. Properties of

**Delay**
are presented below:

The **Delay** component is connected to **Data** to
data one. It stores latest output values of **Data**. The *Step
count* = 4 means that **Delay** stores 4 last values of each
output parameters. The *Formula_4* of data is *Z* coordinate of
satellite. So all parameters of **Delay** are considered as
functions of *Z*. Let us consider all components of forecast. The **
Satellite** component is a container which contains **Motion
equations** of the satellite. The **Data** component is
connected to **Motion equations** and adds time parameters to
motion parameters. Properties of **Data** are presented below:

.

The **Recursive** component is similar to
Memory component of Simulink. This component calculates
time delay of *Z* coordinate. Properties of the **Recursive**
element are presented below:

The **Condition** element is used for determination of time of
equator intersection. Properties of **Condition** are presented
below:

Meaning of parameters of this component is contained in comments:

And at last, **Output** component contains calculation of forecast
parameters. It has the following formulae:

The 86 400 number is number of seconds in a day. The *time* function
converts `double`

variable to `DateTime`

. The *b*
is condition of equator intersection. Input parameters are motion parameters as
functions of *Z*. Full list of parameters is contained in the following
comments:

And at last, **Chart** component has the following properties:

These properties have the following meaning. Output is performed when condition
variable is `true`

. In this case, condition is *Formula_1* of
**Condition**

object. It is condition of equator
intersection. Output parameters are *Formula_1* - *Formula_7* of
**Output**

object. Labels *X*, *Y*, *
Z*, *Vx*, *Vy*, *Vz* are labels which are reflected in
XML document. The XML document is presented below:

Collapse | Copy Code
<Root>
<Parameters>
<Parameter Name="T" Value="Monday, June 28, 1999 11:17:05 PM.457" />
<Parameter Name="X" Value="-6595.47050815637" />
<Parameter Name="Y" Value="-2472.05799683873" />
<Parameter Name="Z" Value="0" />
<Parameter Name="Vx" Value="-0.541295154046453" />
<Parameter Name="Vy" Value="1.46945520971716" />
<Parameter Name="Vz" Value="7.45051367374592" />
</Parameters>
<Parameters>
<Parameter Name="T" Value="Tuesday, June 29, 1999 12:55:08 AM.068" />
<Parameter Name="X" Value="-7026.76544757067" />
<Parameter Name="Y" Value="487.053173194772" />
<Parameter Name="Z" Value="0" />
<Parameter Name="Vx" Value="0.117122882887633" />
<Parameter Name="Vy" Value="1.56173832654579" />
<Parameter Name="Vz" Value="7.45055871464937" />
</Parameters>
<Root>

The first parameter has `DateTime`

type and the other ones have

double

type. The XML document reflects this circumstance. The

XSLT (Extensible Stylesheet Language
Transformations) is used for generation of documents. The following code
contains XSLT file.

Collapse | Copy Code
<xsl:stylesheet version="1.0" xmlns:xsl=http://www.w3.org/1999/XSL/Transform
xmlns:msxsl="urn:schemas-microsoft-com:xslt"
xmlns:user="urn:my-scripts">
<xsl:template match="/">
<html>
<body>
<p>
<h1>Forecast</h1>
</p>
<xsl:apply-templates />
</body>
</html>
</xsl:template>
<xsl:template match="Parameters">
<p></p>
<p>
<table border="1">
<xsl:apply-templates />
</table>
</p>
</xsl:template>
<xsl:template match="Parameter">
<xsl:apply-templates />
<tr>
<td>
<xsl:value-of select="@Name" />
</td>
<td>
<xsl:value-of select="@Value" />
</td>
</tr>
</xsl:template>
</xsl:stylesheet>

This XSLT code provides the following HTML document.

T | Monday, June 28, 1999 11:17:05 PM.457 |

X | -6595.47050815637 |

Y | -2472.05799683873 |

Z | 0 |

Vx | -0.541295154046453 |

Vy | 1.46945520971716 |

Vz | 7.45051367374592 |

T | Tuesday, June 29, 1999 12:55:08 AM.068 |

X | -7026.76544757067 |

Y | 487.053173194772 |

Z | 0 |

Vx | 0.117122882887633 |

Vy | 1.56173832654579 |

Vz | 7.45055871464937 |

#### 4.2.7 Short instruction

##### 4.2.7.1 Unpack following archive

##### 4.2.7.2 Installation of audio files

Installation of audio files includes following steps.

*Step 1.* Copy `SOUNDS`

directory to any directory.

*Step 2.* Setting directory of unpacked files by following way

##### 4.2.7.3 Installation of containes

Copy `Containers`

directory to directory of

Aviation.exe

file;

##### 4.2.7.4 Start animation

Start

Aviation.exe

. Open

Orbit.cfa

file. Click following

*Animation button*
## Points of Interest

My chief told me: "Do not read smart books. If you continue your reading then you shall have a lot of ill-wishers." Chief was quite right. Really a had a lot of ill-wishers. However I continued reading of smart books.