EN-0001 - Project Initialization

Document Number: EN-0001
Title: Project Initialization
Author: Aamir Khan Pathan
Date Created: 29-06-2026
Revision: 0.1.0
Status: Draft
Subsystem: Project Administration

Purpose

This document formally establishes the ASTRA Autonomous Flight System (AAFS) project and defines its initial engineering vision, objectives, scope, and development philosophy.

This entry serves as the foundation of the engineering notebook and provides the baseline from which all future technical decisions, requirements, and design work will evolve.

Project Name

ASTRA Autonomous Flight System
AAFS

Vision

ASTRA is intended to become a modular autonomous flight platform capable of collecting telemetry, estimating vehicle state, executing autonomous guidance algorithms and corrections, and supporting progressively advanced recovery capabilities.

The project is designed as a long-term engineering initiative focused on learning and applying principles from:

Aerospace Engineering
Systems Engineering
Embedded Systems
Flight Software
Electronics
Control Theory
Navigation
Software Engineering

The emphasis is placed on designing every subsystem as an independent module while maintaining full system integration through well-defined interfaces.

Primary Objectives

The initial goals of ASTRA are:

Develop a complete systems engineering workflow.
Design a modular avionics architecture.
Build a scalable flight software framework.
Develop a desktop Ground Control Station.
Create a complete engineering notebook documenting every design decision.
Validate all major subsystems through simulation before hardware implementation.
Support future autonomous navigation and controlled recovery.

Engineering Philosophy

ASTRA follows several core principles:

Safety before capability.
Documentation before implementation.
Simulation before hardware.
Modularity over complexity.
Verification before validation.
Continuous improvement.

Every engineering decision should and shall be justified through analysis, testing, or documented trade studies.

Long-Term Development Phases

Phase I

Project Planning
Repository
Documentation
Architecture
Simulation

Phase II

Avionics
Flight Computer
Telemetry
Ground Station

Phase III

Navigation
Sensor Fusion
Guidance
Flight Control
Recovery

Phase IV

Integrated Testing
Hardware
Simulation
Flight Testing
Mission Operations

Success Criteria

The ASTRA project will be considered successful if it achieves:

Comprehensive engineering documentation.
Modular subsystem architecture.
Repeatable verification procedures.
Reliable software architecture.
Successful integrated subsystem operation.
Continuous engineering improvement through iterative development.

Notes

This engineering notebook shall record every major engineering decision, design revision, analysis, simulation, trade study, and test result produced throughout the ASTRA project lifecycle.

Each notebook entry should provide sufficient technical detail to allow another engineer to understand the reasoning behind the decisions made.